design_id,animals,traits,animal_count,trait_count,empty_mass_kg,payload_mass_kg,rotor_count,max_twr,burst_power_factor,burst_duration_s,unsteady_lift_gain,energy_system_type,energy_system_description,energy_density_class,power_class,tech_maturity_class,energy_system_extra_failure_risk,battery_mass_kg,battery_spec_energy_Wh_per_kg,battery_energy_Wh,supercap_mass_kg,supercap_energy_Wh,structural_material,structural_material_class,structural_extra_failure_risk,rotor_blade_material,landing_gear_material,frame_stiffness_longitudinal,tendon_cable_fraction,gust_rejection_gain,landing_gear_mass_kg,max_touchdown_velocity_mps,cruise_speed_mps,climb_rate_mps,mode_count,mtow_kg,payload_to_aircraft_ratio,rule_empty_mass_ok,rule_payload_ok,design_qualifying,design_qualifying_score,design_summary,propulsion_architecture,primary_propulsor_type,secondary_propulsor_type,secondary_propulsor_fraction,propulsion_hover_power_factor,propulsion_cruise_power_factor,propulsion_arch_extra_failure_risk,image_prompt
DLIFT_dd2199576a,harpy_eagle,"LIFT_BURST_POWER,LIFT_HIGH_CONTINUOUS,PAYLOAD_CENTRAL_TALON",1,3,21.26938124699791,57.34675561410429,8,2.1310596998296174,2.3533989748458226,18.16705265098237,0.0,li_ion,"Conventional high-TRL Li-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,6.797296377167434,182.38377755504564,1239.716590429023,0.6559139244108101,26.236556976432404,aluminum_lithium,medium_stiff,0.02,carbon_composite,titanium,0.7549191064456662,0.0,1.3174122209048251,1.2715421771424384,1.6785313677518174,21.188609133556533,2.025995038712244,3,78.6161368611022,2.6962117490934796,True,True,True,2.6962117490934796,"Bio-inspired by harpy_eagle, this design is a heavy-lift VTOL rotorcraft concept. It uses 8 rotors, has an empty mass of 21.3 kg, and is configured to carry a payload of 57.3 kg (2.70:1 payload-to-aircraft mass ratio). The primary energy system is li-ion with a battery pack of 6.8 kg (~1240 Wh usable). It also incorporates approximately 0.7 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses aluminum lithium (medium_stiff), with carbon_composite rotor blades and titanium landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; strong continuous lifting capacity for heavy payloads; a central, talon-like payload cradle aligned with the center of gravity. In the synthetic DARPA Lift mission model, it cruises at about 21.2 m/s and climbs at roughly 2.0 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 2.70. ",rotor_plus_pusher,multirotor,pusher_propeller,0.33610020660719675,1.05,0.9,0.01,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by harpy_eagle, with 8 evenly spaced rotors and a compact central fuselage. Sleek aluminum lithium airframe, carbon composite rotor blades, and rugged titanium landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_b752d6fd53,osprey,"PAYLOAD_DAMPED,PAYLOAD_SLING_LOAD,STAB_GUST_REJECTION",1,3,18.676748462871352,57.34432775454279,18,1.631237618460707,1.0,0.0,0.0,fuel_cell_li_ion_hybrid,"Hybrid hydrogen fuel-cell plus Li-ion buffer pack, high effective energy but complex and less mature.",extreme,medium_low,medium_low,0.06,8.759997838686836,622.7798975098585,5455.55055616397,2.053842752969624,82.15371011878496,steel_truss,heavy_robust,0.01,glass_composite,titanium,0.33859367926946776,0.0,1.2,1.8682209856894476,0.9219656871726529,23.85819428670109,5.505470505890676,4,76.02107621741413,3.07035926882782,True,True,True,3.07035926882782,"Bio-inspired by osprey, this design is a heavy-lift VTOL rotorcraft concept. It uses 18 rotors, has an empty mass of 18.7 kg, and is configured to carry a payload of 57.3 kg (3.07:1 payload-to-aircraft mass ratio). The primary energy system is fuel-cell-li-ion-hybrid with a battery pack of 8.8 kg (~5456 Wh usable). It also incorporates approximately 2.1 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses steel truss (heavy_robust), with glass_composite rotor blades and titanium landing gear. Key bio-inspired features include damped payload mounting to reduce oscillations during flight; a sling-load style payload mount hanging beneath the airframe; enhanced gust rejection and stability control for windy conditions. In the synthetic DARPA Lift mission model, it cruises at about 23.9 m/s and climbs at roughly 5.5 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.07. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by osprey, with 18 evenly spaced rotors and a compact central fuselage. Sleek steel truss airframe, glass composite rotor blades, and rugged titanium landing gear. Subtle external cues of a fuel-cell-li-ion-hybrid energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_78409336d9,"tiger,osprey,dragonfly","LIFT_BURST_POWER,PAYLOAD_DAMPED,PAYLOAD_SLING_LOAD,STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION,STRUCT_ROBUST_GEAR,STRUCT_TENDON_CABLES",3,7,23.407847991810257,76.11555709510301,13,2.2783370874414537,2.0153257639552686,6.381488730000461,0.0,li_ion,"Conventional high-TRL Li-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,4.45394132177838,256.2799798122802,1141.455992030444,2.767302241854824,110.69208967419297,steel_truss,heavy_robust,0.01,carbon_composite,steel,0.3972227781108579,0.25408653702665346,1.9779820684157183,5.184990434192323,1.4683569310141764,9.817431848944661,4.2694277747556395,2,99.52340508691327,3.2517110125515893,True,True,True,3.2517110125515893,"Bio-inspired by tiger, osprey, dragonfly, this design is a heavy-lift VTOL rotorcraft concept. It uses 13 rotors, has an empty mass of 23.4 kg, and is configured to carry a payload of 76.1 kg (3.25:1 payload-to-aircraft mass ratio). The primary energy system is li-ion with a battery pack of 4.5 kg (~1141 Wh usable). It also incorporates approximately 2.8 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses steel truss (heavy_robust), with carbon_composite rotor blades and steel landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; damped payload mounting to reduce oscillations during flight; a sling-load style payload mount hanging beneath the airframe; many smaller rotors for fine-grained control and redundancy; enhanced gust rejection and stability control for windy conditions. In the synthetic DARPA Lift mission model, it cruises at about 9.8 m/s and climbs at roughly 4.3 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.25. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by tiger, osprey, dragonfly, with 13 evenly spaced rotors and a compact central fuselage. Sleek steel truss airframe, carbon composite rotor blades, and rugged steel landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_777c41302d,"tiger,osprey","LIFT_BURST_POWER,PAYLOAD_DAMPED,PAYLOAD_SLING_LOAD,STAB_GUST_REJECTION,STRUCT_ROBUST_GEAR,STRUCT_TENDON_CABLES",2,6,21.041907073512135,76.47149225422213,22,1.7617394368365118,2.5692388485815068,16.727448962032938,0.0,li_ion,"Conventional high-TRL Li-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,3.87237732805941,214.4840945925102,830.5633451293863,1.2707358690597623,50.82943476239049,aluminum_lithium,medium_stiff,0.02,glass_composite,steel,0.9889156479561763,0.06889250980637121,1.2,2.025070942658845,3.335017609058373,9.973126678405713,2.760835633763246,5,97.51339932773426,3.63424721851783,True,True,True,3.63424721851783,"Bio-inspired by tiger, osprey, this design is a heavy-lift VTOL rotorcraft concept. It uses 22 rotors, has an empty mass of 21.0 kg, and is configured to carry a payload of 76.5 kg (3.63:1 payload-to-aircraft mass ratio). The primary energy system is li-ion with a battery pack of 3.9 kg (~831 Wh usable). It also incorporates approximately 1.3 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses aluminum lithium (medium_stiff), with glass_composite rotor blades and steel landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; damped payload mounting to reduce oscillations during flight; a sling-load style payload mount hanging beneath the airframe; enhanced gust rejection and stability control for windy conditions; reinforced landing gear designed to tolerate higher touchdown loads. In the synthetic DARPA Lift mission model, it cruises at about 10.0 m/s and climbs at roughly 2.8 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.63. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by tiger, osprey, with 22 evenly spaced rotors and a compact central fuselage. Sleek aluminum lithium airframe, glass composite rotor blades, and rugged steel landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_a5ffc698c7,bee,"LIFT_UNSTEADY_AERO,STAB_DISTRIBUTED_THRUST",1,2,12.714565911343538,67.52532783376914,20,2.3871419831649057,1.0,0.0,0.13278153381763533,li_ion,"Conventional high-TRL Li-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,7.570456472940767,248.10740362752972,1878.2862997765599,0.0,0.0,carbon_composite,light_stiff,0.01,carbon_composite,composite,0.6409071745150736,0.0,1.9123941908436342,2.2444775419352827,1.6578381150144212,5.7948332457812874,2.327933621979502,6,80.23989374511268,5.310863800196683,True,True,True,5.310863800196683,"Bio-inspired by bee, this design is a heavy-lift VTOL rotorcraft concept. It uses 20 rotors, has an empty mass of 12.7 kg, and is configured to carry a payload of 67.5 kg (5.31:1 payload-to-aircraft mass ratio). The primary energy system is li-ion with a battery pack of 7.6 kg (~1878 Wh usable). The main load-bearing frame uses carbon composite (light_stiff), with carbon_composite rotor blades and composite landing gear. Key bio-inspired features include unsteady aerodynamics (insect-like vortex lift) for better hover and low-speed lift; many smaller rotors for fine-grained control and redundancy. In the synthetic DARPA Lift mission model, it cruises at about 5.8 m/s and climbs at roughly 2.3 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 5.31. ",rotor_plus_pusher,multirotor,pusher_propeller,0.32654793839069085,1.05,0.9,0.01,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by bee, with 20 evenly spaced rotors and a compact central fuselage. Sleek carbon composite airframe, carbon composite rotor blades, and rugged composite landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_9833ba6e1e,"golden_eagle,tiger,bee","LIFT_BURST_POWER,LIFT_HIGH_CONTINUOUS,LIFT_UNSTEADY_AERO,PAYLOAD_CENTRAL_TALON,STAB_DISTRIBUTED_THRUST,STRUCT_ROBUST_GEAR,STRUCT_TENDON_CABLES",3,7,18.9152955110602,58.17044636944449,23,1.3948815167297204,1.6857605755865173,14.68745118962262,0.21322820384797433,li_ion,"Conventional high-TRL Li-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,5.260091268629047,252.65272369748575,1328.9763859164918,0.15239668098759196,6.095867239503678,titanium_alloy,heavy_robust,0.005,glass_composite,titanium,0.6135130135770959,0.09157376249119158,1.969696930743254,1.534373160420386,2.0755065355825515,19.113348935199816,4.2436274590989855,2,77.08574188050468,3.0753125868655298,True,True,True,3.0753125868655298,"Bio-inspired by golden_eagle, tiger, bee, this design is a heavy-lift VTOL rotorcraft concept. It uses 23 rotors, has an empty mass of 18.9 kg, and is configured to carry a payload of 58.2 kg (3.08:1 payload-to-aircraft mass ratio). The primary energy system is li-ion with a battery pack of 5.3 kg (~1329 Wh usable). It also incorporates approximately 0.2 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses titanium alloy (heavy_robust), with glass_composite rotor blades and titanium landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; strong continuous lifting capacity for heavy payloads; unsteady aerodynamics (insect-like vortex lift) for better hover and low-speed lift; a central, talon-like payload cradle aligned with the center of gravity; many smaller rotors for fine-grained control and redundancy. In the synthetic DARPA Lift mission model, it cruises at about 19.1 m/s and climbs at roughly 4.2 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.08. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by golden_eagle, tiger, bee, with 23 evenly spaced rotors and a compact central fuselage. Sleek titanium alloy airframe, glass composite rotor blades, and rugged titanium landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_fb955dc7d6,bat,"WING_FOLDABLE,WING_MORPHING_MEMBRANE",1,2,22.90208478632612,75.75779754013345,11,1.3794019620360527,1.0,0.0,0.0,fuel_cell_li_ion_hybrid,"Hybrid hydrogen fuel-cell plus Li-ion buffer pack, high effective energy but complex and less mature.",extreme,medium_low,medium_low,0.06,6.1469258200132675,728.2145523886247,4476.280834587042,2.613969107589025,104.55876430356099,carbon_composite,light_stiff,0.01,glass_composite,steel,0.5445243569877131,0.0,0.60413113199423,2.885978907937137,1.2022922581655044,15.188113510560747,4.718072473441055,6,98.65988232645958,3.307899619049759,True,True,True,3.307899619049759,"Bio-inspired by bat, this design is a heavy-lift VTOL rotorcraft concept. It uses 11 rotors, has an empty mass of 22.9 kg, and is configured to carry a payload of 75.8 kg (3.31:1 payload-to-aircraft mass ratio). The primary energy system is fuel-cell-li-ion-hybrid with a battery pack of 6.1 kg (~4476 Wh usable). It also incorporates approximately 2.6 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses carbon composite (light_stiff), with glass_composite rotor blades and steel landing gear. Key bio-inspired features include foldable wings that deploy after vertical takeoff for cruise efficiency; morphing membrane-like lifting surfaces that can change area and camber. In the synthetic DARPA Lift mission model, it cruises at about 15.2 m/s and climbs at roughly 4.7 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.31. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by bat, with 11 evenly spaced rotors and a compact central fuselage. Sleek carbon composite airframe, glass composite rotor blades, and rugged steel landing gear. Subtle external cues of a fuel-cell-li-ion-hybrid energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_df3892a379,"osprey,albatross,cheetah,bee,bat","LIFT_BURST_POWER,LIFT_ENERGY_DENSE,LIFT_UNSTEADY_AERO,MISSION_GLIDE_SEGMENTS,MISSION_MULTI_GAIT,PAYLOAD_DAMPED,PAYLOAD_SLING_LOAD,STAB_COMPLIANT_SPINE,STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION,STRUCT_TENDON_CABLES,WING_FOLDABLE,WING_HIGH_ASPECT,WING_MORPHING_MEMBRANE",5,14,20.46647431590916,77.08416637197747,23,1.8967473568121331,1.8121503375163257,17.173327878168976,0.07596873731708845,li_ion,"Conventional high-TRL Li-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,10.07182944729822,228.53292563838102,2301.7446501218606,0.9667476892096144,38.66990756838457,aluminum_lithium,medium_stiff,0.02,glass_composite,steel,0.7,0.6718824025781254,1.6039421689103326,2.8059776074944764,1.0675728099860549,18.277076726099974,4.477043221449502,4,97.55064068788664,3.7663627443666643,True,True,True,3.7663627443666643,"Bio-inspired by osprey, albatross, cheetah, bee, bat, this design is a heavy-lift VTOL rotorcraft concept. It uses 23 rotors, has an empty mass of 20.5 kg, and is configured to carry a payload of 77.1 kg (3.77:1 payload-to-aircraft mass ratio). The primary energy system is li-ion with a battery pack of 10.1 kg (~2302 Wh usable). It also incorporates approximately 1.0 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses aluminum lithium (medium_stiff), with glass_composite rotor blades and steel landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; an emphasis on energy-dense storage for long-range flight; unsteady aerodynamics (insect-like vortex lift) for better hover and low-speed lift; mission planning that includes partial-power or glide segments to save energy; multiple flight modes (hover, heavy-load cruise, light-load return, etc.). In the synthetic DARPA Lift mission model, it cruises at about 18.3 m/s and climbs at roughly 4.5 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.77. ",rotor_plus_small_jet,multirotor,small_jet,0.3253414412622197,1.15,0.85,0.03,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by osprey, albatross, cheetah, bee, bat, with 23 evenly spaced rotors and a compact central fuselage. Sleek aluminum lithium airframe, glass composite rotor blades, and rugged steel landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_9419c53a79,"tiger,bat,cheetah,dragonfly","LIFT_BURST_POWER,MISSION_MULTI_GAIT,STAB_COMPLIANT_SPINE,STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION,STRUCT_ROBUST_GEAR,STRUCT_TENDON_CABLES,WING_FOLDABLE,WING_MORPHING_MEMBRANE",4,9,17.573920150958756,54.77473722628998,19,1.7300976601456715,2.5035535730010228,17.277669093312653,0.0,li_ion,"Conventional high-TRL Li-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,9.999073518005746,218.76776136562134,2187.474929264385,0.7177375914438986,28.709503657755945,aluminum_lithium,medium_stiff,0.02,glass_composite,titanium,0.5350932756349197,0.6251187829532218,1.2,1.2334887636549636,1.8991058772940144,8.056105331542959,2.8558115084239497,5,72.34865737724874,3.116819511854998,True,True,True,3.116819511854998,"Bio-inspired by tiger, bat, cheetah, dragonfly, this design is a heavy-lift VTOL rotorcraft concept. It uses 19 rotors, has an empty mass of 17.6 kg, and is configured to carry a payload of 54.8 kg (3.12:1 payload-to-aircraft mass ratio). The primary energy system is li-ion with a battery pack of 10.0 kg (~2187 Wh usable). It also incorporates approximately 0.7 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses aluminum lithium (medium_stiff), with glass_composite rotor blades and titanium landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; multiple flight modes (hover, heavy-load cruise, light-load return, etc.); a compliant spine-like frame that absorbs dynamic loads; many smaller rotors for fine-grained control and redundancy; enhanced gust rejection and stability control for windy conditions. In the synthetic DARPA Lift mission model, it cruises at about 8.1 m/s and climbs at roughly 2.9 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.12. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by tiger, bat, cheetah, dragonfly, with 19 evenly spaced rotors and a compact central fuselage. Sleek aluminum lithium airframe, glass composite rotor blades, and rugged titanium landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_dd0dee3314,"harpy_eagle,golden_eagle,bee,albatross,cheetah","LIFT_BURST_POWER,LIFT_ENERGY_DENSE,LIFT_HIGH_CONTINUOUS,LIFT_UNSTEADY_AERO,MISSION_GLIDE_SEGMENTS,MISSION_MULTI_GAIT,PAYLOAD_CENTRAL_TALON,STAB_COMPLIANT_SPINE,STAB_DISTRIBUTED_THRUST,STRUCT_TENDON_CABLES,WING_HIGH_ASPECT",5,11,22.835641944939127,55.45187079540297,12,1.6307454098633953,1.423320568422963,8.556378682982245,0.19030742697350678,li_ion,"Conventional high-TRL Li-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,9.768088411993062,246.5539428124218,2408.360711717218,0.7568145953471418,30.27258381388567,carbon_composite,light_stiff,0.01,carbon_composite,steel,0.7,0.24497224060412873,1.4752161398748125,2.910884106274319,1.8035093104877788,20.084664081190525,5.798446930863955,4,78.2875127403421,2.4283035672527835,True,True,True,2.4283035672527835,"Bio-inspired by harpy_eagle, golden_eagle, bee, albatross, cheetah, this design is a heavy-lift VTOL rotorcraft concept. It uses 12 rotors, has an empty mass of 22.8 kg, and is configured to carry a payload of 55.5 kg (2.43:1 payload-to-aircraft mass ratio). The primary energy system is li-ion with a battery pack of 9.8 kg (~2408 Wh usable). It also incorporates approximately 0.8 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses carbon composite (light_stiff), with carbon_composite rotor blades and steel landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; an emphasis on energy-dense storage for long-range flight; strong continuous lifting capacity for heavy payloads; unsteady aerodynamics (insect-like vortex lift) for better hover and low-speed lift; mission planning that includes partial-power or glide segments to save energy. In the synthetic DARPA Lift mission model, it cruises at about 20.1 m/s and climbs at roughly 5.8 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 2.43. ",rotor_plus_small_jet,multirotor,small_jet,0.28640069697584736,1.15,0.85,0.03,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by harpy_eagle, golden_eagle, bee, albatross, cheetah, with 12 evenly spaced rotors and a compact central fuselage. Sleek carbon composite airframe, carbon composite rotor blades, and rugged steel landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_dcf6b4e522,tiger,"LIFT_BURST_POWER,STRUCT_ROBUST_GEAR,STRUCT_TENDON_CABLES",1,3,20.094290675710063,50.37956450497559,17,2.2512632853260817,1.2110777412879972,19.333388642647837,0.0,li_ion,"Conventional high-TRL Li-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,10.458365799022124,236.58469149648616,2474.2892461190513,1.306461435023031,52.258457400921245,magnesium_alloy,very_light_fragile,0.04,aluminum,titanium,0.7791655078482562,0.37672103451377903,1.225246255824794,2.065000940023902,2.943078642915367,10.367910760984508,5.406852640077327,2,70.47385518068566,2.5071581434757637,True,True,True,2.5071581434757637,"Bio-inspired by tiger, this design is a heavy-lift VTOL rotorcraft concept. It uses 17 rotors, has an empty mass of 20.1 kg, and is configured to carry a payload of 50.4 kg (2.51:1 payload-to-aircraft mass ratio). The primary energy system is li-ion with a battery pack of 10.5 kg (~2474 Wh usable). It also incorporates approximately 1.3 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses magnesium alloy (very_light_fragile), with aluminum rotor blades and titanium landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; reinforced landing gear designed to tolerate higher touchdown loads; a tendon/cable-based structural system to save mass in tension members. In the synthetic DARPA Lift mission model, it cruises at about 10.4 m/s and climbs at roughly 5.4 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 2.51. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by tiger, with 17 evenly spaced rotors and a compact central fuselage. Sleek magnesium alloy airframe, aluminum rotor blades, and rugged titanium landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_9a7d8977d2,"bee,tiger,cheetah,albatross,osprey","LIFT_BURST_POWER,LIFT_ENERGY_DENSE,LIFT_UNSTEADY_AERO,MISSION_GLIDE_SEGMENTS,MISSION_MULTI_GAIT,PAYLOAD_DAMPED,PAYLOAD_SLING_LOAD,STAB_COMPLIANT_SPINE,STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION,STRUCT_ROBUST_GEAR,STRUCT_TENDON_CABLES,WING_HIGH_ASPECT",5,13,15.83278739186038,56.916141238955234,10,1.5417671216083813,2.485762127278208,19.16491852668839,0.1725408885351379,li_ion,"Conventional high-TRL Li-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,9.647441881580555,202.11997015749515,1949.9406652012306,1.7687607178823725,70.7504287152949,magnesium_alloy,very_light_fragile,0.04,carbon_composite,composite,0.7,0.20737252428560113,1.2,1.589095291946155,2.874055457133094,7.531659196959632,2.1820628039328733,4,72.74892863081561,3.594827608701154,True,True,True,3.594827608701154,"Bio-inspired by bee, tiger, cheetah, albatross, osprey, this design is a heavy-lift VTOL rotorcraft concept. It uses 10 rotors, has an empty mass of 15.8 kg, and is configured to carry a payload of 56.9 kg (3.59:1 payload-to-aircraft mass ratio). The primary energy system is li-ion with a battery pack of 9.6 kg (~1950 Wh usable). It also incorporates approximately 1.8 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses magnesium alloy (very_light_fragile), with carbon_composite rotor blades and composite landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; an emphasis on energy-dense storage for long-range flight; unsteady aerodynamics (insect-like vortex lift) for better hover and low-speed lift; mission planning that includes partial-power or glide segments to save energy; multiple flight modes (hover, heavy-load cruise, light-load return, etc.). In the synthetic DARPA Lift mission model, it cruises at about 7.5 m/s and climbs at roughly 2.2 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.59. ",rotor_plus_pusher,multirotor,pusher_propeller,0.4789669571640778,1.05,0.9,0.01,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by bee, tiger, cheetah, albatross, osprey, with 10 evenly spaced rotors and a compact central fuselage. Sleek magnesium alloy airframe, carbon composite rotor blades, and rugged composite landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_20b3d95319,"golden_eagle,albatross,bee,tiger,osprey","LIFT_BURST_POWER,LIFT_ENERGY_DENSE,LIFT_HIGH_CONTINUOUS,LIFT_UNSTEADY_AERO,MISSION_GLIDE_SEGMENTS,PAYLOAD_CENTRAL_TALON,PAYLOAD_DAMPED,PAYLOAD_SLING_LOAD,STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION,STRUCT_ROBUST_GEAR,STRUCT_TENDON_CABLES,WING_HIGH_ASPECT",5,13,20.255351714900456,54.711712801426316,9,1.8727891438088626,1.3130652308862762,9.944798735220452,0.17234278394619224,li_ion,"Conventional high-TRL Li-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,3.2937586984283187,203.04839116749514,668.7924046098129,0.8481551193368633,33.92620477347453,steel_truss,heavy_robust,0.01,carbon_composite,titanium,0.5094476498592913,0.553873421531473,1.3846843838078868,5.169325014336628,1.3434576412693926,7.295526049220915,2.8992378010640953,3,74.96706451632677,2.7010991253821923,True,True,True,2.7010991253821923,"Bio-inspired by golden_eagle, albatross, bee, tiger, osprey, this design is a heavy-lift VTOL rotorcraft concept. It uses 9 rotors, has an empty mass of 20.3 kg, and is configured to carry a payload of 54.7 kg (2.70:1 payload-to-aircraft mass ratio). The primary energy system is li-ion with a battery pack of 3.3 kg (~669 Wh usable). It also incorporates approximately 0.8 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses steel truss (heavy_robust), with carbon_composite rotor blades and titanium landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; an emphasis on energy-dense storage for long-range flight; strong continuous lifting capacity for heavy payloads; unsteady aerodynamics (insect-like vortex lift) for better hover and low-speed lift; mission planning that includes partial-power or glide segments to save energy. In the synthetic DARPA Lift mission model, it cruises at about 7.3 m/s and climbs at roughly 2.9 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 2.70. ",ducted_fans_hybrid,ducted_fan_array,none,0.0,0.95,1.05,0.015,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by golden_eagle, albatross, bee, tiger, osprey, with 9 evenly spaced rotors and a compact central fuselage. Sleek steel truss airframe, carbon composite rotor blades, and rugged titanium landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_c7b1f338f6,"golden_eagle,cheetah,osprey,albatross","LIFT_BURST_POWER,LIFT_ENERGY_DENSE,LIFT_HIGH_CONTINUOUS,MISSION_GLIDE_SEGMENTS,MISSION_MULTI_GAIT,PAYLOAD_CENTRAL_TALON,PAYLOAD_DAMPED,PAYLOAD_SLING_LOAD,STAB_COMPLIANT_SPINE,STAB_GUST_REJECTION,STRUCT_TENDON_CABLES,WING_HIGH_ASPECT",4,12,16.16635492081365,70.10400528563557,9,1.5617251290105516,2.387347347966865,7.899702521144748,0.0,fuel_cell_li_ion_hybrid,"Hybrid hydrogen fuel-cell plus Li-ion buffer pack, high effective energy but complex and less mature.",extreme,medium_low,medium_low,0.06,10.322094312641752,620.0386435887132,6400.0973566051625,1.3644777258051883,54.57910903220753,aluminum_lithium,medium_stiff,0.02,carbon_composite,composite,0.5829225399005219,0.36021737663037356,1.982178822172631,2.8018113526909514,1.58518718871439,13.264951415986431,2.7503301655781085,4,86.27036020644921,4.336413844000107,True,True,True,4.336413844000107,"Bio-inspired by golden_eagle, cheetah, osprey, albatross, this design is a heavy-lift VTOL rotorcraft concept. It uses 9 rotors, has an empty mass of 16.2 kg, and is configured to carry a payload of 70.1 kg (4.34:1 payload-to-aircraft mass ratio). The primary energy system is fuel-cell-li-ion-hybrid with a battery pack of 10.3 kg (~6400 Wh usable). It also incorporates approximately 1.4 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses aluminum lithium (medium_stiff), with carbon_composite rotor blades and composite landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; an emphasis on energy-dense storage for long-range flight; strong continuous lifting capacity for heavy payloads; mission planning that includes partial-power or glide segments to save energy; multiple flight modes (hover, heavy-load cruise, light-load return, etc.). In the synthetic DARPA Lift mission model, it cruises at about 13.3 m/s and climbs at roughly 2.8 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 4.34. ",rotor_plus_pusher,multirotor,pusher_propeller,0.39939724095287543,1.05,0.9,0.01,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by golden_eagle, cheetah, osprey, albatross, with 9 evenly spaced rotors and a compact central fuselage. Sleek aluminum lithium airframe, carbon composite rotor blades, and rugged composite landing gear. Subtle external cues of a fuel-cell-li-ion-hybrid energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_39f9665e8c,"bee,dragonfly,bat,harpy_eagle","LIFT_BURST_POWER,LIFT_HIGH_CONTINUOUS,LIFT_UNSTEADY_AERO,PAYLOAD_CENTRAL_TALON,STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION,WING_FOLDABLE,WING_MORPHING_MEMBRANE",4,8,15.535487291035333,58.956675493153014,22,1.9118927374367658,2.319881506109839,17.709430109904126,0.11163684826079862,li_ion,"Conventional high-TRL Li-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,5.991959601396744,241.02981420959833,1444.2409094760762,1.1316301626416578,45.26520650566631,steel_truss,heavy_robust,0.01,aluminum,composite,0.49052207496219324,0.0,1.2,4.544859040742572,1.3215501910991563,11.363526544675997,3.8919050009616574,5,74.49216278418835,3.7949678943880722,True,True,True,3.7949678943880722,"Bio-inspired by bee, dragonfly, bat, harpy_eagle, this design is a heavy-lift VTOL rotorcraft concept. It uses 22 rotors, has an empty mass of 15.5 kg, and is configured to carry a payload of 59.0 kg (3.79:1 payload-to-aircraft mass ratio). The primary energy system is li-ion with a battery pack of 6.0 kg (~1444 Wh usable). It also incorporates approximately 1.1 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses steel truss (heavy_robust), with aluminum rotor blades and composite landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; strong continuous lifting capacity for heavy payloads; unsteady aerodynamics (insect-like vortex lift) for better hover and low-speed lift; a central, talon-like payload cradle aligned with the center of gravity; many smaller rotors for fine-grained control and redundancy. In the synthetic DARPA Lift mission model, it cruises at about 11.4 m/s and climbs at roughly 3.9 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.79. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by bee, dragonfly, bat, harpy_eagle, with 22 evenly spaced rotors and a compact central fuselage. Sleek steel truss airframe, aluminum rotor blades, and rugged composite landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_3feeb6a466,"albatross,golden_eagle,tiger","LIFT_BURST_POWER,LIFT_ENERGY_DENSE,LIFT_HIGH_CONTINUOUS,MISSION_GLIDE_SEGMENTS,PAYLOAD_CENTRAL_TALON,STRUCT_ROBUST_GEAR,STRUCT_TENDON_CABLES,WING_HIGH_ASPECT",3,8,24.229221602756823,72.81109078982796,7,1.7211499723263881,2.388002325586469,18.358209054858264,0.0,li_ion,"Conventional high-TRL Li-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,10.165291186459907,203.4694220772167,2068.325922955622,1.1245232693259446,44.980930773037784,carbon_composite,light_stiff,0.01,carbon_composite,steel,0.9402399948883339,0.11898855434766815,0.618452525989992,3.8317736828775515,2.609131105612246,9.816595837126261,5.651316064094219,3,97.04031239258478,3.0050940960292114,True,True,True,3.0050940960292114,"Bio-inspired by albatross, golden_eagle, tiger, this design is a heavy-lift VTOL rotorcraft concept. It uses 7 rotors, has an empty mass of 24.2 kg, and is configured to carry a payload of 72.8 kg (3.01:1 payload-to-aircraft mass ratio). The primary energy system is li-ion with a battery pack of 10.2 kg (~2068 Wh usable). It also incorporates approximately 1.1 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses carbon composite (light_stiff), with carbon_composite rotor blades and steel landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; an emphasis on energy-dense storage for long-range flight; strong continuous lifting capacity for heavy payloads; mission planning that includes partial-power or glide segments to save energy; a central, talon-like payload cradle aligned with the center of gravity. In the synthetic DARPA Lift mission model, it cruises at about 9.8 m/s and climbs at roughly 5.7 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.01. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by albatross, golden_eagle, tiger, with 7 evenly spaced rotors and a compact central fuselage. Sleek carbon composite airframe, carbon composite rotor blades, and rugged steel landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_7e1fec7931,"albatross,bee,golden_eagle","LIFT_BURST_POWER,LIFT_ENERGY_DENSE,LIFT_HIGH_CONTINUOUS,LIFT_UNSTEADY_AERO,MISSION_GLIDE_SEGMENTS,PAYLOAD_CENTRAL_TALON,STAB_DISTRIBUTED_THRUST,WING_HIGH_ASPECT",3,8,19.95772347507365,68.62673489390912,8,1.9795473451616576,2.8068074081459358,13.987790351138887,0.07723322098815902,li_ion,"Conventional high-TRL Li-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,8.216164248315625,238.58878143513905,1960.2846160765803,0.2704001272386568,10.816005089546273,carbon_composite,light_stiff,0.01,glass_composite,titanium,0.4317630442650234,0.0,1.3091116384766317,3.510192180815721,1.56170474740557,23.26973948963394,5.321890478269589,4,88.58445836898277,3.4386053589539407,True,True,True,3.4386053589539407,"Bio-inspired by albatross, bee, golden_eagle, this design is a heavy-lift VTOL rotorcraft concept. It uses 8 rotors, has an empty mass of 20.0 kg, and is configured to carry a payload of 68.6 kg (3.44:1 payload-to-aircraft mass ratio). The primary energy system is li-ion with a battery pack of 8.2 kg (~1960 Wh usable). It also incorporates approximately 0.3 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses carbon composite (light_stiff), with glass_composite rotor blades and titanium landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; an emphasis on energy-dense storage for long-range flight; strong continuous lifting capacity for heavy payloads; unsteady aerodynamics (insect-like vortex lift) for better hover and low-speed lift; mission planning that includes partial-power or glide segments to save energy. In the synthetic DARPA Lift mission model, it cruises at about 23.3 m/s and climbs at roughly 5.3 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.44. ",ducted_fans_hybrid,ducted_fan_array,none,0.0,0.95,1.05,0.015,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by albatross, bee, golden_eagle, with 8 evenly spaced rotors and a compact central fuselage. Sleek carbon composite airframe, glass composite rotor blades, and rugged titanium landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_64d4c0476d,"golden_eagle,osprey,harpy_eagle,bat","LIFT_BURST_POWER,LIFT_HIGH_CONTINUOUS,PAYLOAD_CENTRAL_TALON,PAYLOAD_DAMPED,PAYLOAD_SLING_LOAD,STAB_GUST_REJECTION,WING_FOLDABLE,WING_MORPHING_MEMBRANE",4,8,15.804557304450064,64.77873856934617,7,1.4287200454038609,2.0750932117650516,9.606979129552423,0.0,li_ion,"Conventional high-TRL Li-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,11.544426915707149,235.71871933101062,2721.237527980938,1.6205774862869102,64.82309945147641,titanium_alloy,heavy_robust,0.005,glass_composite,composite,0.8722121274822383,0.0,1.7505396249444822,3.1857392990148568,2.3781061314273106,10.594802801715772,4.761122654990254,3,80.58329587379623,4.0987379349819895,True,True,True,4.0987379349819895,"Bio-inspired by golden_eagle, osprey, harpy_eagle, bat, this design is a heavy-lift VTOL rotorcraft concept. It uses 7 rotors, has an empty mass of 15.8 kg, and is configured to carry a payload of 64.8 kg (4.10:1 payload-to-aircraft mass ratio). The primary energy system is li-ion with a battery pack of 11.5 kg (~2721 Wh usable). It also incorporates approximately 1.6 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses titanium alloy (heavy_robust), with glass_composite rotor blades and composite landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; strong continuous lifting capacity for heavy payloads; a central, talon-like payload cradle aligned with the center of gravity; damped payload mounting to reduce oscillations during flight; a sling-load style payload mount hanging beneath the airframe. In the synthetic DARPA Lift mission model, it cruises at about 10.6 m/s and climbs at roughly 4.8 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 4.10. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by golden_eagle, osprey, harpy_eagle, bat, with 7 evenly spaced rotors and a compact central fuselage. Sleek titanium alloy airframe, glass composite rotor blades, and rugged composite landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_bd0b347916,osprey,"PAYLOAD_DAMPED,PAYLOAD_SLING_LOAD,STAB_GUST_REJECTION",1,3,12.18575409038386,73.69953992704262,11,1.9243940908706192,1.0,0.0,0.0,li_ion,"Conventional high-TRL Li-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,5.38830757492476,190.14068349702242,1024.5364851883774,0.0,0.0,aluminum_lithium,medium_stiff,0.02,carbon_composite,titanium,0.6137926499889188,0.0,1.2,2.577831062538095,1.4040108398175044,9.4309951283657,4.460427345137746,6,85.88529401742647,6.0480081397015155,True,True,True,6.0480081397015155,"Bio-inspired by osprey, this design is a heavy-lift VTOL rotorcraft concept. It uses 11 rotors, has an empty mass of 12.2 kg, and is configured to carry a payload of 73.7 kg (6.05:1 payload-to-aircraft mass ratio). The primary energy system is li-ion with a battery pack of 5.4 kg (~1025 Wh usable). The main load-bearing frame uses aluminum lithium (medium_stiff), with carbon_composite rotor blades and titanium landing gear. Key bio-inspired features include damped payload mounting to reduce oscillations during flight; a sling-load style payload mount hanging beneath the airframe; enhanced gust rejection and stability control for windy conditions. In the synthetic DARPA Lift mission model, it cruises at about 9.4 m/s and climbs at roughly 4.5 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 6.05. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by osprey, with 11 evenly spaced rotors and a compact central fuselage. Sleek aluminum lithium airframe, carbon composite rotor blades, and rugged titanium landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_a9c8632f25,"bat,bee,cheetah","LIFT_BURST_POWER,LIFT_UNSTEADY_AERO,MISSION_MULTI_GAIT,STAB_COMPLIANT_SPINE,STAB_DISTRIBUTED_THRUST,STRUCT_TENDON_CABLES,WING_FOLDABLE,WING_MORPHING_MEMBRANE",3,8,15.18612245603474,78.60777552857374,19,1.193986631391307,2.663543776949709,4.584911728962516,0.024141108141446405,li_s,Experimental lithium-sulfur chemistry with very high energy density but lower maturity and stability.,very_high,medium,low,0.05,10.305923567496531,383.4556103423025,3951.8642117155023,1.7593952482184307,70.37580992873723,titanium_alloy,heavy_robust,0.005,carbon_composite,titanium,0.6296464541051829,0.46573836400204077,1.6254263753772173,4.245987025250073,1.9421213574922989,24.36797250622949,4.401640364898708,4,93.79389798460848,5.176290113302502,True,True,True,5.176290113302502,"Bio-inspired by bat, bee, cheetah, this design is a heavy-lift VTOL rotorcraft concept. It uses 19 rotors, has an empty mass of 15.2 kg, and is configured to carry a payload of 78.6 kg (5.18:1 payload-to-aircraft mass ratio). The primary energy system is li-s with a battery pack of 10.3 kg (~3952 Wh usable). It also incorporates approximately 1.8 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses titanium alloy (heavy_robust), with carbon_composite rotor blades and titanium landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; unsteady aerodynamics (insect-like vortex lift) for better hover and low-speed lift; multiple flight modes (hover, heavy-load cruise, light-load return, etc.); a compliant spine-like frame that absorbs dynamic loads; many smaller rotors for fine-grained control and redundancy. In the synthetic DARPA Lift mission model, it cruises at about 24.4 m/s and climbs at roughly 4.4 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 5.18. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by bat, bee, cheetah, with 19 evenly spaced rotors and a compact central fuselage. Sleek titanium alloy airframe, carbon composite rotor blades, and rugged titanium landing gear. Subtle external cues of a li-s energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_1ab65330ec,"bee,osprey,cheetah,bat","LIFT_BURST_POWER,LIFT_UNSTEADY_AERO,MISSION_MULTI_GAIT,PAYLOAD_DAMPED,PAYLOAD_SLING_LOAD,STAB_COMPLIANT_SPINE,STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION,STRUCT_TENDON_CABLES,WING_FOLDABLE,WING_MORPHING_MEMBRANE",4,11,21.019949596783412,73.30506859900223,22,1.9347132810871293,2.7666843690366867,5.644858357876302,0.18860896978124636,li_ion,"Conventional high-TRL Li-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,3.7342337477872185,215.44903794642607,804.5370684278333,1.2720443193389857,50.881772773559426,titanium_alloy,heavy_robust,0.005,carbon_composite,titanium,0.7,0.2416209988366033,1.2,3.4485151503208447,1.6862685007845275,15.538682142962896,3.2336775674050258,4,94.32501819578565,3.48740458493867,True,True,True,3.48740458493867,"Bio-inspired by bee, osprey, cheetah, bat, this design is a heavy-lift VTOL rotorcraft concept. It uses 22 rotors, has an empty mass of 21.0 kg, and is configured to carry a payload of 73.3 kg (3.49:1 payload-to-aircraft mass ratio). The primary energy system is li-ion with a battery pack of 3.7 kg (~805 Wh usable). It also incorporates approximately 1.3 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses titanium alloy (heavy_robust), with carbon_composite rotor blades and titanium landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; unsteady aerodynamics (insect-like vortex lift) for better hover and low-speed lift; multiple flight modes (hover, heavy-load cruise, light-load return, etc.); damped payload mounting to reduce oscillations during flight; a sling-load style payload mount hanging beneath the airframe. In the synthetic DARPA Lift mission model, it cruises at about 15.5 m/s and climbs at roughly 3.2 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.49. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by bee, osprey, cheetah, bat, with 22 evenly spaced rotors and a compact central fuselage. Sleek titanium alloy airframe, carbon composite rotor blades, and rugged titanium landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_040032b0e1,"golden_eagle,bat,cheetah","LIFT_BURST_POWER,LIFT_HIGH_CONTINUOUS,MISSION_MULTI_GAIT,PAYLOAD_CENTRAL_TALON,STAB_COMPLIANT_SPINE,STRUCT_TENDON_CABLES,WING_FOLDABLE,WING_MORPHING_MEMBRANE",3,8,13.323289167444825,63.070295808212,16,1.8335475602008842,1.791533393718666,8.274667551209642,0.0,li_ion,"Conventional high-TRL Li-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,5.997617602438188,193.45061664365494,1160.2428235845068,1.531449853626445,61.25799414505779,carbon_composite,light_stiff,0.01,carbon_composite,composite,0.5990189544137328,0.509165373971733,1.728422902287278,3.0173665681125446,0.9725376978934486,7.928884365553888,2.789087211295933,6,76.39358497565682,4.733838244862457,True,True,True,4.733838244862457,"Bio-inspired by golden_eagle, bat, cheetah, this design is a heavy-lift VTOL rotorcraft concept. It uses 16 rotors, has an empty mass of 13.3 kg, and is configured to carry a payload of 63.1 kg (4.73:1 payload-to-aircraft mass ratio). The primary energy system is li-ion with a battery pack of 6.0 kg (~1160 Wh usable). It also incorporates approximately 1.5 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses carbon composite (light_stiff), with carbon_composite rotor blades and composite landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; strong continuous lifting capacity for heavy payloads; multiple flight modes (hover, heavy-load cruise, light-load return, etc.); a central, talon-like payload cradle aligned with the center of gravity; a compliant spine-like frame that absorbs dynamic loads. In the synthetic DARPA Lift mission model, it cruises at about 7.9 m/s and climbs at roughly 2.8 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 4.73. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by golden_eagle, bat, cheetah, with 16 evenly spaced rotors and a compact central fuselage. Sleek carbon composite airframe, carbon composite rotor blades, and rugged composite landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_b3d767778b,cheetah,"LIFT_BURST_POWER,MISSION_MULTI_GAIT,STAB_COMPLIANT_SPINE,STRUCT_TENDON_CABLES",1,4,23.363124457170805,67.14970059361401,10,1.5501374680325997,1.951258055886139,5.564638303825856,0.0,li_ion,"Conventional high-TRL Li-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,3.9315168954335244,251.93014671646188,990.4676282848166,1.0303133275148029,41.21253310059211,magnesium_alloy,very_light_fragile,0.04,carbon_composite,titanium,0.426078545866919,0.30643079201646306,1.1591326876439365,1.9801754049149982,0.8174924159630828,12.457039642026542,3.1315743144576715,5,90.51282505078481,2.874174672857331,True,True,True,2.874174672857331,"Bio-inspired by cheetah, this design is a heavy-lift VTOL rotorcraft concept. It uses 10 rotors, has an empty mass of 23.4 kg, and is configured to carry a payload of 67.1 kg (2.87:1 payload-to-aircraft mass ratio). The primary energy system is li-ion with a battery pack of 3.9 kg (~990 Wh usable). It also incorporates approximately 1.0 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses magnesium alloy (very_light_fragile), with carbon_composite rotor blades and titanium landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; multiple flight modes (hover, heavy-load cruise, light-load return, etc.); a compliant spine-like frame that absorbs dynamic loads; a tendon/cable-based structural system to save mass in tension members. In the synthetic DARPA Lift mission model, it cruises at about 12.5 m/s and climbs at roughly 3.1 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 2.87. ",rotor_plus_small_jet,multirotor,small_jet,0.30366931616787435,1.15,0.85,0.03,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by cheetah, with 10 evenly spaced rotors and a compact central fuselage. Sleek magnesium alloy airframe, carbon composite rotor blades, and rugged titanium landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_6f353f5dac,"cheetah,albatross,golden_eagle","LIFT_BURST_POWER,LIFT_ENERGY_DENSE,LIFT_HIGH_CONTINUOUS,MISSION_GLIDE_SEGMENTS,MISSION_MULTI_GAIT,PAYLOAD_CENTRAL_TALON,STAB_COMPLIANT_SPINE,STRUCT_TENDON_CABLES,WING_HIGH_ASPECT",3,9,24.499707763787857,54.64835518833215,13,2.282199744160237,1.2022815273357883,16.104870246172716,0.0,solid_state,Solid-state battery with improved safety and energy density but still under active development.,high,medium,medium_low,0.03,10.953139489433054,263.3972743121805,2885.027086677775,1.0102931158928445,40.41172463571378,magnesium_alloy,very_light_fragile,0.04,carbon_composite,steel,0.3722157436157238,0.5819415396823878,1.6566467205964825,2.8319050659269207,0.8310783314881174,13.753468102766934,3.643434445986134,4,79.14806295212,2.2305717160065854,True,True,True,2.2305717160065854,"Bio-inspired by cheetah, albatross, golden_eagle, this design is a heavy-lift VTOL rotorcraft concept. It uses 13 rotors, has an empty mass of 24.5 kg, and is configured to carry a payload of 54.6 kg (2.23:1 payload-to-aircraft mass ratio). The primary energy system is solid-state with a battery pack of 11.0 kg (~2885 Wh usable). It also incorporates approximately 1.0 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses magnesium alloy (very_light_fragile), with carbon_composite rotor blades and steel landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; an emphasis on energy-dense storage for long-range flight; strong continuous lifting capacity for heavy payloads; mission planning that includes partial-power or glide segments to save energy; multiple flight modes (hover, heavy-load cruise, light-load return, etc.). In the synthetic DARPA Lift mission model, it cruises at about 13.8 m/s and climbs at roughly 3.6 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 2.23. ",ducted_fans_hybrid,ducted_fan_array,none,0.0,0.95,1.05,0.015,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by cheetah, albatross, golden_eagle, with 13 evenly spaced rotors and a compact central fuselage. Sleek magnesium alloy airframe, carbon composite rotor blades, and rugged steel landing gear. Subtle external cues of a solid-state energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_81509a2b4b,albatross,"LIFT_ENERGY_DENSE,MISSION_GLIDE_SEGMENTS,WING_HIGH_ASPECT",1,3,22.208790698193756,76.53889321154023,4,1.6808556681466076,1.0,0.0,0.0,li_ion,"Conventional high-TRL Li-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,6.365653389111181,210.8932894435676,1342.4735826872513,0.0,0.0,carbon_composite,light_stiff,0.01,carbon_composite,titanium,0.40629400578264696,0.0,1.572056408784844,1.5061646211359574,0.7920986136436401,5.7660638223408744,5.669584686451005,5,98.74768390973398,3.446333222356188,True,True,True,3.446333222356188,"Bio-inspired by albatross, this design is a heavy-lift VTOL rotorcraft concept. It uses 4 rotors, has an empty mass of 22.2 kg, and is configured to carry a payload of 76.5 kg (3.45:1 payload-to-aircraft mass ratio). The primary energy system is li-ion with a battery pack of 6.4 kg (~1342 Wh usable). The main load-bearing frame uses carbon composite (light_stiff), with carbon_composite rotor blades and titanium landing gear. Key bio-inspired features include an emphasis on energy-dense storage for long-range flight; mission planning that includes partial-power or glide segments to save energy; long, high-aspect-ratio lifting surfaces for efficient cruise. In the synthetic DARPA Lift mission model, it cruises at about 5.8 m/s and climbs at roughly 5.7 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.45. ",rotor_plus_pusher,multirotor,pusher_propeller,0.2555170767272745,1.05,0.9,0.01,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by albatross, with 4 evenly spaced rotors and a compact central fuselage. Sleek carbon composite airframe, carbon composite rotor blades, and rugged titanium landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_11fef36c93,"cheetah,harpy_eagle,bee,albatross","LIFT_BURST_POWER,LIFT_ENERGY_DENSE,LIFT_HIGH_CONTINUOUS,LIFT_UNSTEADY_AERO,MISSION_GLIDE_SEGMENTS,MISSION_MULTI_GAIT,PAYLOAD_CENTRAL_TALON,STAB_COMPLIANT_SPINE,STAB_DISTRIBUTED_THRUST,STRUCT_TENDON_CABLES,WING_HIGH_ASPECT",4,11,24.262992781894503,57.60950783207638,4,1.5999314271206262,1.1351191154837978,7.099140714555959,0.16427610000270784,li_ion,"Conventional high-TRL Li-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,8.23712989402326,240.53431411535655,1981.3123893379845,0.40022876957809206,16.009150783123683,aluminum_lithium,medium_stiff,0.02,carbon_composite,steel,0.7,0.47927779648628843,1.9712287786832738,2.174859100662734,0.8645559968277465,7.6970516239256455,4.864180230384779,5,81.87250061397089,2.374377652004483,True,True,True,2.374377652004483,"Bio-inspired by cheetah, harpy_eagle, bee, albatross, this design is a heavy-lift VTOL rotorcraft concept. It uses 4 rotors, has an empty mass of 24.3 kg, and is configured to carry a payload of 57.6 kg (2.37:1 payload-to-aircraft mass ratio). The primary energy system is li-ion with a battery pack of 8.2 kg (~1981 Wh usable). It also incorporates approximately 0.4 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses aluminum lithium (medium_stiff), with carbon_composite rotor blades and steel landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; an emphasis on energy-dense storage for long-range flight; strong continuous lifting capacity for heavy payloads; unsteady aerodynamics (insect-like vortex lift) for better hover and low-speed lift; mission planning that includes partial-power or glide segments to save energy. In the synthetic DARPA Lift mission model, it cruises at about 7.7 m/s and climbs at roughly 4.9 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 2.37. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by cheetah, harpy_eagle, bee, albatross, with 4 evenly spaced rotors and a compact central fuselage. Sleek aluminum lithium airframe, carbon composite rotor blades, and rugged steel landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_c2f9f4a59d,"dragonfly,cheetah,tiger","LIFT_BURST_POWER,MISSION_MULTI_GAIT,STAB_COMPLIANT_SPINE,STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION,STRUCT_ROBUST_GEAR,STRUCT_TENDON_CABLES",3,7,20.97078639139571,54.99934316197741,18,1.5921657772807891,1.084710325700259,17.790631975958668,0.0,li_ion,"Conventional high-TRL Li-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,11.983355379957441,201.9644288059886,2420.211524492275,2.9400818375828375,117.6032735033135,steel_truss,heavy_robust,0.01,carbon_composite,steel,0.582033681028472,0.5607671828935189,1.5191159117220348,5.982230103686659,1.1783384050876493,17.151458066417106,5.125247878973866,4,75.97012955337311,2.6226647935598435,True,True,True,2.6226647935598435,"Bio-inspired by dragonfly, cheetah, tiger, this design is a heavy-lift VTOL rotorcraft concept. It uses 18 rotors, has an empty mass of 21.0 kg, and is configured to carry a payload of 55.0 kg (2.62:1 payload-to-aircraft mass ratio). The primary energy system is li-ion with a battery pack of 12.0 kg (~2420 Wh usable). It also incorporates approximately 2.9 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses steel truss (heavy_robust), with carbon_composite rotor blades and steel landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; multiple flight modes (hover, heavy-load cruise, light-load return, etc.); a compliant spine-like frame that absorbs dynamic loads; many smaller rotors for fine-grained control and redundancy; enhanced gust rejection and stability control for windy conditions. In the synthetic DARPA Lift mission model, it cruises at about 17.2 m/s and climbs at roughly 5.1 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 2.62. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by dragonfly, cheetah, tiger, with 18 evenly spaced rotors and a compact central fuselage. Sleek steel truss airframe, carbon composite rotor blades, and rugged steel landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_1dad3769e7,"bee,golden_eagle,dragonfly","LIFT_BURST_POWER,LIFT_HIGH_CONTINUOUS,LIFT_UNSTEADY_AERO,PAYLOAD_CENTRAL_TALON,STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION",3,6,18.77714201531953,76.73995047061666,9,2.096532745610098,2.8546489134463555,13.840900383588277,0.19842409596125068,li_ion,"Conventional high-TRL Li-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,4.092262095706112,196.07842969421486,802.4043256232113,0.4166306161150972,16.66522464460389,magnesium_alloy,very_light_fragile,0.04,carbon_composite,steel,0.5024140342657691,0.0,1.7054925894328796,2.0661496284311216,1.7238967252410418,6.724309633038654,3.2371628701138486,5,95.51709248593619,4.086881294715008,True,True,True,4.086881294715008,"Bio-inspired by bee, golden_eagle, dragonfly, this design is a heavy-lift VTOL rotorcraft concept. It uses 9 rotors, has an empty mass of 18.8 kg, and is configured to carry a payload of 76.7 kg (4.09:1 payload-to-aircraft mass ratio). The primary energy system is li-ion with a battery pack of 4.1 kg (~802 Wh usable). It also incorporates approximately 0.4 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses magnesium alloy (very_light_fragile), with carbon_composite rotor blades and steel landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; strong continuous lifting capacity for heavy payloads; unsteady aerodynamics (insect-like vortex lift) for better hover and low-speed lift; a central, talon-like payload cradle aligned with the center of gravity; many smaller rotors for fine-grained control and redundancy. In the synthetic DARPA Lift mission model, it cruises at about 6.7 m/s and climbs at roughly 3.2 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 4.09. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by bee, golden_eagle, dragonfly, with 9 evenly spaced rotors and a compact central fuselage. Sleek magnesium alloy airframe, carbon composite rotor blades, and rugged steel landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_39c05f3bbc,"osprey,bee","LIFT_UNSTEADY_AERO,PAYLOAD_DAMPED,PAYLOAD_SLING_LOAD,STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION",2,5,22.531625051417365,66.90854103293887,4,1.213711996850718,1.0,0.0,0.23713671349259788,li_s,Experimental lithium-sulfur chemistry with very high energy density but lower maturity and stability.,very_high,medium,low,0.05,5.38190317049749,331.62125695529465,1784.7534942120633,0.0,0.0,titanium_alloy,heavy_robust,0.005,glass_composite,titanium,1.060642489566408,0.0,1.3183662253209014,3.296010615065178,1.1041882259092453,9.897558212978861,5.22939725771519,5,89.44016608435624,2.969539075865722,True,True,True,2.969539075865722,"Bio-inspired by osprey, bee, this design is a heavy-lift VTOL rotorcraft concept. It uses 4 rotors, has an empty mass of 22.5 kg, and is configured to carry a payload of 66.9 kg (2.97:1 payload-to-aircraft mass ratio). The primary energy system is li-s with a battery pack of 5.4 kg (~1785 Wh usable). The main load-bearing frame uses titanium alloy (heavy_robust), with glass_composite rotor blades and titanium landing gear. Key bio-inspired features include unsteady aerodynamics (insect-like vortex lift) for better hover and low-speed lift; damped payload mounting to reduce oscillations during flight; a sling-load style payload mount hanging beneath the airframe; many smaller rotors for fine-grained control and redundancy; enhanced gust rejection and stability control for windy conditions. In the synthetic DARPA Lift mission model, it cruises at about 9.9 m/s and climbs at roughly 5.2 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 2.97. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by osprey, bee, with 4 evenly spaced rotors and a compact central fuselage. Sleek titanium alloy airframe, glass composite rotor blades, and rugged titanium landing gear. Subtle external cues of a li-s energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_49d1b3fa8b,"tiger,cheetah,golden_eagle,bat","LIFT_BURST_POWER,LIFT_HIGH_CONTINUOUS,MISSION_MULTI_GAIT,PAYLOAD_CENTRAL_TALON,STAB_COMPLIANT_SPINE,STRUCT_ROBUST_GEAR,STRUCT_TENDON_CABLES,WING_FOLDABLE,WING_MORPHING_MEMBRANE",4,9,19.291801399820958,51.45974398788968,13,1.792851884935247,2.764678952736402,14.122420627123491,0.0,li_ion,"Conventional high-TRL Li-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,7.830216743600343,247.77378923147742,1940.122473065617,1.2927833080426216,51.711332321704866,steel_truss,heavy_robust,0.01,glass_composite,composite,0.5839639541004088,0.2804071347103296,1.355422465821544,1.842817948306946,2.409668779863455,6.4706349948568365,4.017022116492819,6,70.75154538771064,2.6674411021236857,True,True,True,2.6674411021236857,"Bio-inspired by tiger, cheetah, golden_eagle, bat, this design is a heavy-lift VTOL rotorcraft concept. It uses 13 rotors, has an empty mass of 19.3 kg, and is configured to carry a payload of 51.5 kg (2.67:1 payload-to-aircraft mass ratio). The primary energy system is li-ion with a battery pack of 7.8 kg (~1940 Wh usable). It also incorporates approximately 1.3 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses steel truss (heavy_robust), with glass_composite rotor blades and composite landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; strong continuous lifting capacity for heavy payloads; multiple flight modes (hover, heavy-load cruise, light-load return, etc.); a central, talon-like payload cradle aligned with the center of gravity; a compliant spine-like frame that absorbs dynamic loads. In the synthetic DARPA Lift mission model, it cruises at about 6.5 m/s and climbs at roughly 4.0 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 2.67. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by tiger, cheetah, golden_eagle, bat, with 13 evenly spaced rotors and a compact central fuselage. Sleek steel truss airframe, glass composite rotor blades, and rugged composite landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_d6f79e1ab2,"dragonfly,harpy_eagle,tiger,albatross","LIFT_BURST_POWER,LIFT_ENERGY_DENSE,LIFT_HIGH_CONTINUOUS,MISSION_GLIDE_SEGMENTS,PAYLOAD_CENTRAL_TALON,STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION,STRUCT_ROBUST_GEAR,STRUCT_TENDON_CABLES,WING_HIGH_ASPECT",4,10,15.319130462321517,69.66772916530907,22,1.9086881542098562,2.4428002245926135,12.919895709809879,0.0,li_ion,"Conventional high-TRL Li-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,8.661227170308273,229.57886444008716,1988.4346984170027,2.523501374874793,100.94005499499173,carbon_composite,light_stiff,0.01,glass_composite,titanium,1.060117981503912,0.07692686493358779,1.2,1.7257575874253326,1.2042937743580362,18.81000521837051,3.6415096372908202,6,84.9868596276306,4.547760027023842,True,True,True,4.547760027023842,"Bio-inspired by dragonfly, harpy_eagle, tiger, albatross, this design is a heavy-lift VTOL rotorcraft concept. It uses 22 rotors, has an empty mass of 15.3 kg, and is configured to carry a payload of 69.7 kg (4.55:1 payload-to-aircraft mass ratio). The primary energy system is li-ion with a battery pack of 8.7 kg (~1988 Wh usable). It also incorporates approximately 2.5 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses carbon composite (light_stiff), with glass_composite rotor blades and titanium landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; an emphasis on energy-dense storage for long-range flight; strong continuous lifting capacity for heavy payloads; mission planning that includes partial-power or glide segments to save energy; a central, talon-like payload cradle aligned with the center of gravity. In the synthetic DARPA Lift mission model, it cruises at about 18.8 m/s and climbs at roughly 3.6 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 4.55. ",ducted_fans_hybrid,ducted_fan_array,none,0.0,0.95,1.05,0.015,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by dragonfly, harpy_eagle, tiger, albatross, with 22 evenly spaced rotors and a compact central fuselage. Sleek carbon composite airframe, glass composite rotor blades, and rugged titanium landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_085a5414c3,"bat,bee,tiger,golden_eagle","LIFT_BURST_POWER,LIFT_HIGH_CONTINUOUS,LIFT_UNSTEADY_AERO,PAYLOAD_CENTRAL_TALON,STAB_DISTRIBUTED_THRUST,STRUCT_ROBUST_GEAR,STRUCT_TENDON_CABLES,WING_FOLDABLE,WING_MORPHING_MEMBRANE",4,9,15.630658149911694,58.6289102484242,6,1.5849089197338633,1.8847522237296708,7.359547583049196,0.1197698157541208,li_ion,"Conventional high-TRL Li-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,7.847201313377875,254.64191470266462,1998.2263674958067,2.088513901940468,83.54055607761872,carbon_composite,light_stiff,0.01,glass_composite,steel,0.5166926895759208,0.46888377542517273,1.2965622345991987,2.95143048748465,0.9074733205183884,13.266027320965172,4.869432225000974,2,74.25956839833589,3.750891976916239,True,True,True,3.750891976916239,"Bio-inspired by bat, bee, tiger, golden_eagle, this design is a heavy-lift VTOL rotorcraft concept. It uses 6 rotors, has an empty mass of 15.6 kg, and is configured to carry a payload of 58.6 kg (3.75:1 payload-to-aircraft mass ratio). The primary energy system is li-ion with a battery pack of 7.8 kg (~1998 Wh usable). It also incorporates approximately 2.1 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses carbon composite (light_stiff), with glass_composite rotor blades and steel landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; strong continuous lifting capacity for heavy payloads; unsteady aerodynamics (insect-like vortex lift) for better hover and low-speed lift; a central, talon-like payload cradle aligned with the center of gravity; many smaller rotors for fine-grained control and redundancy. In the synthetic DARPA Lift mission model, it cruises at about 13.3 m/s and climbs at roughly 4.9 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.75. ",rotor_plus_pusher,multirotor,pusher_propeller,0.2549868136798782,1.05,0.9,0.01,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by bat, bee, tiger, golden_eagle, with 6 evenly spaced rotors and a compact central fuselage. Sleek carbon composite airframe, glass composite rotor blades, and rugged steel landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_bd89c5eb09,"tiger,cheetah,golden_eagle,dragonfly,albatross","LIFT_BURST_POWER,LIFT_ENERGY_DENSE,LIFT_HIGH_CONTINUOUS,MISSION_GLIDE_SEGMENTS,MISSION_MULTI_GAIT,PAYLOAD_CENTRAL_TALON,STAB_COMPLIANT_SPINE,STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION,STRUCT_ROBUST_GEAR,STRUCT_TENDON_CABLES,WING_HIGH_ASPECT",5,12,15.410463518724907,74.26441634729059,14,1.3274919675556343,1.9178289420647223,7.373502963901824,0.0,li_ion,"Conventional high-TRL Li-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,9.629561059430312,243.26141315402046,2342.500631369944,1.703343667262818,68.13374669051272,magnesium_alloy,very_light_fragile,0.04,carbon_composite,composite,0.7,0.5788928776934167,1.272920988439694,0.8196538383586305,2.757767560229863,8.695624020946799,2.5624475025371938,4,89.6748798660155,4.8190903704521,True,True,True,4.8190903704521,"Bio-inspired by tiger, cheetah, golden_eagle, dragonfly, albatross, this design is a heavy-lift VTOL rotorcraft concept. It uses 14 rotors, has an empty mass of 15.4 kg, and is configured to carry a payload of 74.3 kg (4.82:1 payload-to-aircraft mass ratio). The primary energy system is li-ion with a battery pack of 9.6 kg (~2343 Wh usable). It also incorporates approximately 1.7 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses magnesium alloy (very_light_fragile), with carbon_composite rotor blades and composite landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; an emphasis on energy-dense storage for long-range flight; strong continuous lifting capacity for heavy payloads; mission planning that includes partial-power or glide segments to save energy; multiple flight modes (hover, heavy-load cruise, light-load return, etc.). In the synthetic DARPA Lift mission model, it cruises at about 8.7 m/s and climbs at roughly 2.6 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 4.82. ",ducted_fans_hybrid,ducted_fan_array,none,0.0,0.95,1.05,0.015,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by tiger, cheetah, golden_eagle, dragonfly, albatross, with 14 evenly spaced rotors and a compact central fuselage. Sleek magnesium alloy airframe, carbon composite rotor blades, and rugged composite landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_402286448f,"albatross,golden_eagle","LIFT_BURST_POWER,LIFT_ENERGY_DENSE,LIFT_HIGH_CONTINUOUS,MISSION_GLIDE_SEGMENTS,PAYLOAD_CENTRAL_TALON,WING_HIGH_ASPECT",2,6,18.568833202752096,65.8451937221958,15,1.2093438110064163,2.1283374445469496,4.049886808463624,0.0,li_ion,"Conventional high-TRL Li-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,7.549383504833362,225.81613393822917,1704.7725966785085,0.4495571441472429,17.982285765889717,aluminum_lithium,medium_stiff,0.02,carbon_composite,titanium,0.4437810398775531,0.0,1.3747215176615264,0.8182957555809074,1.520750708065669,21.173841663544742,3.813729200719128,6,84.4140269249479,3.5460059877341594,True,True,True,3.5460059877341594,"Bio-inspired by albatross, golden_eagle, this design is a heavy-lift VTOL rotorcraft concept. It uses 15 rotors, has an empty mass of 18.6 kg, and is configured to carry a payload of 65.8 kg (3.55:1 payload-to-aircraft mass ratio). The primary energy system is li-ion with a battery pack of 7.5 kg (~1705 Wh usable). It also incorporates approximately 0.4 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses aluminum lithium (medium_stiff), with carbon_composite rotor blades and titanium landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; an emphasis on energy-dense storage for long-range flight; strong continuous lifting capacity for heavy payloads; mission planning that includes partial-power or glide segments to save energy; a central, talon-like payload cradle aligned with the center of gravity. In the synthetic DARPA Lift mission model, it cruises at about 21.2 m/s and climbs at roughly 3.8 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.55. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by albatross, golden_eagle, with 15 evenly spaced rotors and a compact central fuselage. Sleek aluminum lithium airframe, carbon composite rotor blades, and rugged titanium landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_cf4aede2d3,osprey,"PAYLOAD_DAMPED,PAYLOAD_SLING_LOAD,STAB_GUST_REJECTION",1,3,24.410584700969835,61.791758953521224,8,2.1190013972685793,1.0,0.0,0.0,li_ion,"Conventional high-TRL Li-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,3.03125965450417,181.81882618575733,551.1400722461925,0.0,0.0,carbon_composite,light_stiff,0.01,glass_composite,steel,0.7395888785425043,0.0,1.7350406560636764,1.229662921286893,1.1923194699752535,10.512994555902546,5.749641444540267,2,86.20234365449106,2.531351039332795,True,True,True,2.531351039332795,"Bio-inspired by osprey, this design is a heavy-lift VTOL rotorcraft concept. It uses 8 rotors, has an empty mass of 24.4 kg, and is configured to carry a payload of 61.8 kg (2.53:1 payload-to-aircraft mass ratio). The primary energy system is li-ion with a battery pack of 3.0 kg (~551 Wh usable). The main load-bearing frame uses carbon composite (light_stiff), with glass_composite rotor blades and steel landing gear. Key bio-inspired features include damped payload mounting to reduce oscillations during flight; a sling-load style payload mount hanging beneath the airframe; enhanced gust rejection and stability control for windy conditions. In the synthetic DARPA Lift mission model, it cruises at about 10.5 m/s and climbs at roughly 5.7 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 2.53. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by osprey, with 8 evenly spaced rotors and a compact central fuselage. Sleek carbon composite airframe, glass composite rotor blades, and rugged steel landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_4f04ee0628,"bat,cheetah","LIFT_BURST_POWER,MISSION_MULTI_GAIT,STAB_COMPLIANT_SPINE,STRUCT_TENDON_CABLES,WING_FOLDABLE,WING_MORPHING_MEMBRANE",2,6,12.586051211905687,60.332444893178284,24,2.0398795346440113,2.571609191961036,8.418485774377308,0.0,li_ion,"Conventional high-TRL Li-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,4.342958470426473,210.11681508057057,912.528601833197,2.263248291714376,90.52993166857505,aluminum_lithium,medium_stiff,0.02,glass_composite,titanium,0.7,0.5640433119544208,1.8721117607238582,2.4683508235541822,2.435572377093253,16.145735163985464,2.536371004236312,4,72.91849610508397,4.793596011758416,True,True,True,4.793596011758416,"Bio-inspired by bat, cheetah, this design is a heavy-lift VTOL rotorcraft concept. It uses 24 rotors, has an empty mass of 12.6 kg, and is configured to carry a payload of 60.3 kg (4.79:1 payload-to-aircraft mass ratio). The primary energy system is li-ion with a battery pack of 4.3 kg (~913 Wh usable). It also incorporates approximately 2.3 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses aluminum lithium (medium_stiff), with glass_composite rotor blades and titanium landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; multiple flight modes (hover, heavy-load cruise, light-load return, etc.); a compliant spine-like frame that absorbs dynamic loads; a tendon/cable-based structural system to save mass in tension members; foldable wings that deploy after vertical takeoff for cruise efficiency. In the synthetic DARPA Lift mission model, it cruises at about 16.1 m/s and climbs at roughly 2.5 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 4.79. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by bat, cheetah, with 24 evenly spaced rotors and a compact central fuselage. Sleek aluminum lithium airframe, glass composite rotor blades, and rugged titanium landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_43d3d690a9,"bat,cheetah,dragonfly","LIFT_BURST_POWER,MISSION_MULTI_GAIT,STAB_COMPLIANT_SPINE,STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION,STRUCT_TENDON_CABLES,WING_FOLDABLE,WING_MORPHING_MEMBRANE",3,8,20.10901674993891,59.25266852860785,15,1.8179431560332828,1.9945545862019667,4.676339936613161,0.0,fuel_cell_li_ion_hybrid,"Hybrid hydrogen fuel-cell plus Li-ion buffer pack, high effective energy but complex and less mature.",extreme,medium_low,medium_low,0.06,7.225413798203026,735.8924726254739,5317.127625701842,2.742991496692467,109.71965986769868,aluminum_lithium,medium_stiff,0.02,carbon_composite,steel,0.4548918688213577,0.10214589917178399,1.2,3.771653876037237,1.658285852074801,13.351561471103473,2.609645640736573,4,79.36168527854676,2.9465721405193945,True,True,True,2.9465721405193945,"Bio-inspired by bat, cheetah, dragonfly, this design is a heavy-lift VTOL rotorcraft concept. It uses 15 rotors, has an empty mass of 20.1 kg, and is configured to carry a payload of 59.3 kg (2.95:1 payload-to-aircraft mass ratio). The primary energy system is fuel-cell-li-ion-hybrid with a battery pack of 7.2 kg (~5317 Wh usable). It also incorporates approximately 2.7 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses aluminum lithium (medium_stiff), with carbon_composite rotor blades and steel landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; multiple flight modes (hover, heavy-load cruise, light-load return, etc.); a compliant spine-like frame that absorbs dynamic loads; many smaller rotors for fine-grained control and redundancy; enhanced gust rejection and stability control for windy conditions. In the synthetic DARPA Lift mission model, it cruises at about 13.4 m/s and climbs at roughly 2.6 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 2.95. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by bat, cheetah, dragonfly, with 15 evenly spaced rotors and a compact central fuselage. Sleek aluminum lithium airframe, carbon composite rotor blades, and rugged steel landing gear. Subtle external cues of a fuel-cell-li-ion-hybrid energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_9bbbdec23e,"cheetah,harpy_eagle,tiger,dragonfly","LIFT_BURST_POWER,LIFT_HIGH_CONTINUOUS,MISSION_MULTI_GAIT,PAYLOAD_CENTRAL_TALON,STAB_COMPLIANT_SPINE,STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION,STRUCT_ROBUST_GEAR,STRUCT_TENDON_CABLES",4,9,18.89554451139071,50.355529043836775,20,2.1110698102760095,2.0714762058478495,7.873705121065855,0.0,li_ion,"Conventional high-TRL Li-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,9.280731685953562,214.44585669408303,1990.2144571422332,2.8191357383826383,112.76542953530553,carbon_composite,light_stiff,0.01,aluminum,steel,0.5155460008814013,0.4338465896883546,1.2,1.8797873612529594,3.1348089962504004,6.580384876288708,5.8371911765941205,5,69.25107355522749,2.664941939803915,True,True,True,2.664941939803915,"Bio-inspired by cheetah, harpy_eagle, tiger, dragonfly, this design is a heavy-lift VTOL rotorcraft concept. It uses 20 rotors, has an empty mass of 18.9 kg, and is configured to carry a payload of 50.4 kg (2.66:1 payload-to-aircraft mass ratio). The primary energy system is li-ion with a battery pack of 9.3 kg (~1990 Wh usable). It also incorporates approximately 2.8 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses carbon composite (light_stiff), with aluminum rotor blades and steel landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; strong continuous lifting capacity for heavy payloads; multiple flight modes (hover, heavy-load cruise, light-load return, etc.); a central, talon-like payload cradle aligned with the center of gravity; a compliant spine-like frame that absorbs dynamic loads. In the synthetic DARPA Lift mission model, it cruises at about 6.6 m/s and climbs at roughly 5.8 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 2.66. ",rotor_plus_pusher,multirotor,pusher_propeller,0.5960932126558909,1.05,0.9,0.01,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by cheetah, harpy_eagle, tiger, dragonfly, with 20 evenly spaced rotors and a compact central fuselage. Sleek carbon composite airframe, aluminum rotor blades, and rugged steel landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_cc8918fb8d,"osprey,bat","PAYLOAD_DAMPED,PAYLOAD_SLING_LOAD,STAB_GUST_REJECTION,WING_FOLDABLE,WING_MORPHING_MEMBRANE",2,5,23.610936753166605,58.97830668742588,22,1.4366610720260016,1.0,0.0,0.0,solid_state,Solid-state battery with improved safety and energy density but still under active development.,high,medium,medium_low,0.03,6.502409466306229,340.6873190302448,2215.288448312754,0.0,0.0,aluminum_lithium,medium_stiff,0.02,glass_composite,titanium,0.9919345705398721,0.0,1.5862453551414724,2.252774980732038,2.4486466548719927,6.073928638947872,3.7483530113739967,2,82.58924344059248,2.497923199913529,True,True,True,2.497923199913529,"Bio-inspired by osprey, bat, this design is a heavy-lift VTOL rotorcraft concept. It uses 22 rotors, has an empty mass of 23.6 kg, and is configured to carry a payload of 59.0 kg (2.50:1 payload-to-aircraft mass ratio). The primary energy system is solid-state with a battery pack of 6.5 kg (~2215 Wh usable). The main load-bearing frame uses aluminum lithium (medium_stiff), with glass_composite rotor blades and titanium landing gear. Key bio-inspired features include damped payload mounting to reduce oscillations during flight; a sling-load style payload mount hanging beneath the airframe; enhanced gust rejection and stability control for windy conditions; foldable wings that deploy after vertical takeoff for cruise efficiency; morphing membrane-like lifting surfaces that can change area and camber. In the synthetic DARPA Lift mission model, it cruises at about 6.1 m/s and climbs at roughly 3.7 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 2.50. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by osprey, bat, with 22 evenly spaced rotors and a compact central fuselage. Sleek aluminum lithium airframe, glass composite rotor blades, and rugged titanium landing gear. Subtle external cues of a solid-state energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_f220256632,golden_eagle,"LIFT_BURST_POWER,LIFT_HIGH_CONTINUOUS,PAYLOAD_CENTRAL_TALON",1,3,16.423928591815738,52.79192781379622,23,2.1982142139539302,2.7274363545363833,3.2097904530272254,0.0,li_ion,"Conventional high-TRL Li-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,10.012521950619636,237.9875075227833,2382.8551430451234,1.678609637287428,67.14438549149712,steel_truss,heavy_robust,0.01,carbon_composite,steel,0.818707253968999,0.0,0.7542526178677386,1.8735812840621715,1.0368135942984213,7.918696412930957,2.6688296030365306,4,69.21585640561196,3.2143300866580207,True,True,True,3.2143300866580207,"Bio-inspired by golden_eagle, this design is a heavy-lift VTOL rotorcraft concept. It uses 23 rotors, has an empty mass of 16.4 kg, and is configured to carry a payload of 52.8 kg (3.21:1 payload-to-aircraft mass ratio). The primary energy system is li-ion with a battery pack of 10.0 kg (~2383 Wh usable). It also incorporates approximately 1.7 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses steel truss (heavy_robust), with carbon_composite rotor blades and steel landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; strong continuous lifting capacity for heavy payloads; a central, talon-like payload cradle aligned with the center of gravity. In the synthetic DARPA Lift mission model, it cruises at about 7.9 m/s and climbs at roughly 2.7 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.21. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by golden_eagle, with 23 evenly spaced rotors and a compact central fuselage. Sleek steel truss airframe, carbon composite rotor blades, and rugged steel landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_01bad8f2d8,"bee,golden_eagle,dragonfly,cheetah","LIFT_BURST_POWER,LIFT_HIGH_CONTINUOUS,LIFT_UNSTEADY_AERO,MISSION_MULTI_GAIT,PAYLOAD_CENTRAL_TALON,STAB_COMPLIANT_SPINE,STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION,STRUCT_TENDON_CABLES",4,9,19.40283792812982,66.36887256352466,21,1.1376825521454696,2.454426727617118,19.030573562102315,0.05241209909032088,li_s,Experimental lithium-sulfur chemistry with very high energy density but lower maturity and stability.,very_high,medium,low,0.05,10.48153627839325,310.37380079064394,3253.194252849934,2.5433637901169845,101.73455160467938,magnesium_alloy,very_light_fragile,0.04,glass_composite,titanium,0.4607845647817353,0.17687717945176415,1.2,1.6838056664727878,1.253981636076646,13.981334416672677,4.39173541901215,6,85.77171049165449,3.420575526598843,True,True,True,3.420575526598843,"Bio-inspired by bee, golden_eagle, dragonfly, cheetah, this design is a heavy-lift VTOL rotorcraft concept. It uses 21 rotors, has an empty mass of 19.4 kg, and is configured to carry a payload of 66.4 kg (3.42:1 payload-to-aircraft mass ratio). The primary energy system is li-s with a battery pack of 10.5 kg (~3253 Wh usable). It also incorporates approximately 2.5 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses magnesium alloy (very_light_fragile), with glass_composite rotor blades and titanium landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; strong continuous lifting capacity for heavy payloads; unsteady aerodynamics (insect-like vortex lift) for better hover and low-speed lift; multiple flight modes (hover, heavy-load cruise, light-load return, etc.); a central, talon-like payload cradle aligned with the center of gravity. In the synthetic DARPA Lift mission model, it cruises at about 14.0 m/s and climbs at roughly 4.4 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.42. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by bee, golden_eagle, dragonfly, cheetah, with 21 evenly spaced rotors and a compact central fuselage. Sleek magnesium alloy airframe, glass composite rotor blades, and rugged titanium landing gear. Subtle external cues of a li-s energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_6fb5b521c3,dragonfly,"STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION",1,2,17.199692856571406,78.85183597039911,7,2.263844842589994,1.0,0.0,0.0,li_s,Experimental lithium-sulfur chemistry with very high energy density but lower maturity and stability.,very_high,medium,low,0.05,6.1349578708932775,351.46000212654394,2156.1923063504087,0.0,0.0,magnesium_alloy,very_light_fragile,0.04,carbon_composite,titanium,0.33150250960919664,0.0,1.5829909149195618,1.7710303999390877,0.6343486800829183,5.893661053506422,4.843115959021009,2,96.05152882697051,4.584490934108312,True,True,True,4.584490934108312,"Bio-inspired by dragonfly, this design is a heavy-lift VTOL rotorcraft concept. It uses 7 rotors, has an empty mass of 17.2 kg, and is configured to carry a payload of 78.9 kg (4.58:1 payload-to-aircraft mass ratio). The primary energy system is li-s with a battery pack of 6.1 kg (~2156 Wh usable). The main load-bearing frame uses magnesium alloy (very_light_fragile), with carbon_composite rotor blades and titanium landing gear. Key bio-inspired features include many smaller rotors for fine-grained control and redundancy; enhanced gust rejection and stability control for windy conditions. In the synthetic DARPA Lift mission model, it cruises at about 5.9 m/s and climbs at roughly 4.8 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 4.58. ",rotor_plus_small_jet,multirotor,small_jet,0.29439097518331414,1.15,0.85,0.03,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by dragonfly, with 7 evenly spaced rotors and a compact central fuselage. Sleek magnesium alloy airframe, carbon composite rotor blades, and rugged titanium landing gear. Subtle external cues of a li-s energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_6bab92a407,"osprey,dragonfly,cheetah,bat","LIFT_BURST_POWER,MISSION_MULTI_GAIT,PAYLOAD_DAMPED,PAYLOAD_SLING_LOAD,STAB_COMPLIANT_SPINE,STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION,STRUCT_TENDON_CABLES,WING_FOLDABLE,WING_MORPHING_MEMBRANE",4,10,13.059399607787848,54.01843308952132,7,1.4340018170143067,1.233897807941504,9.34620320639328,0.0,li_ion,"Conventional high-TRL Li-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,6.496169423789918,227.71406539551452,1479.2691489892393,1.7244181346232432,68.97672538492972,aluminum_lithium,medium_stiff,0.02,carbon_composite,steel,0.7,0.6514864563936716,1.2,1.0840293333958617,1.0776695480986913,8.741971599248053,5.367940856546192,6,67.07783269730916,4.136364206001319,True,True,True,4.136364206001319,"Bio-inspired by osprey, dragonfly, cheetah, bat, this design is a heavy-lift VTOL rotorcraft concept. It uses 7 rotors, has an empty mass of 13.1 kg, and is configured to carry a payload of 54.0 kg (4.14:1 payload-to-aircraft mass ratio). The primary energy system is li-ion with a battery pack of 6.5 kg (~1479 Wh usable). It also incorporates approximately 1.7 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses aluminum lithium (medium_stiff), with carbon_composite rotor blades and steel landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; multiple flight modes (hover, heavy-load cruise, light-load return, etc.); damped payload mounting to reduce oscillations during flight; a sling-load style payload mount hanging beneath the airframe; a compliant spine-like frame that absorbs dynamic loads. In the synthetic DARPA Lift mission model, it cruises at about 8.7 m/s and climbs at roughly 5.4 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 4.14. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by osprey, dragonfly, cheetah, bat, with 7 evenly spaced rotors and a compact central fuselage. Sleek aluminum lithium airframe, carbon composite rotor blades, and rugged steel landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_a9508852b1,"dragonfly,harpy_eagle","LIFT_BURST_POWER,LIFT_HIGH_CONTINUOUS,PAYLOAD_CENTRAL_TALON,STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION",2,5,17.62165428538017,60.457309304669415,6,1.7146978647366662,2.987915368637234,16.185738047973153,0.0,li_ion,"Conventional high-TRL Li-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,10.296324451554693,227.03391175814485,2337.614816967497,1.051892523341969,42.07570093367876,magnesium_alloy,very_light_fragile,0.04,glass_composite,titanium,0.3577180285338689,0.0,1.2,1.0406545942365037,0.6187156672786822,12.01630957905662,3.124340075160792,6,78.07896359004958,3.4308532176135076,True,True,True,3.4308532176135076,"Bio-inspired by dragonfly, harpy_eagle, this design is a heavy-lift VTOL rotorcraft concept. It uses 6 rotors, has an empty mass of 17.6 kg, and is configured to carry a payload of 60.5 kg (3.43:1 payload-to-aircraft mass ratio). The primary energy system is li-ion with a battery pack of 10.3 kg (~2338 Wh usable). It also incorporates approximately 1.1 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses magnesium alloy (very_light_fragile), with glass_composite rotor blades and titanium landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; strong continuous lifting capacity for heavy payloads; a central, talon-like payload cradle aligned with the center of gravity; many smaller rotors for fine-grained control and redundancy; enhanced gust rejection and stability control for windy conditions. In the synthetic DARPA Lift mission model, it cruises at about 12.0 m/s and climbs at roughly 3.1 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.43. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by dragonfly, harpy_eagle, with 6 evenly spaced rotors and a compact central fuselage. Sleek magnesium alloy airframe, glass composite rotor blades, and rugged titanium landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_547070580e,cheetah,"LIFT_BURST_POWER,MISSION_MULTI_GAIT,STAB_COMPLIANT_SPINE,STRUCT_TENDON_CABLES",1,4,19.93550681920199,70.91866933365674,6,2.2139490973069833,1.7954317363773276,19.458185861289,0.0,solid_state,Solid-state battery with improved safety and energy density but still under active development.,high,medium,medium_low,0.03,7.452434527999397,289.05786346309577,2154.18480226211,0.8507792280112612,34.03116912045044,aluminum_lithium,medium_stiff,0.02,carbon_composite,composite,0.7,0.6259082606269891,1.6433810336337529,0.6608002398052182,1.752359044311788,21.7340435772511,2.0651254094909777,4,90.85417615285873,3.5574048845022332,True,True,True,3.5574048845022332,"Bio-inspired by cheetah, this design is a heavy-lift VTOL rotorcraft concept. It uses 6 rotors, has an empty mass of 19.9 kg, and is configured to carry a payload of 70.9 kg (3.56:1 payload-to-aircraft mass ratio). The primary energy system is solid-state with a battery pack of 7.5 kg (~2154 Wh usable). It also incorporates approximately 0.9 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses aluminum lithium (medium_stiff), with carbon_composite rotor blades and composite landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; multiple flight modes (hover, heavy-load cruise, light-load return, etc.); a compliant spine-like frame that absorbs dynamic loads; a tendon/cable-based structural system to save mass in tension members. In the synthetic DARPA Lift mission model, it cruises at about 21.7 m/s and climbs at roughly 2.1 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.56. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by cheetah, with 6 evenly spaced rotors and a compact central fuselage. Sleek aluminum lithium airframe, carbon composite rotor blades, and rugged composite landing gear. Subtle external cues of a solid-state energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_e0bc1b6c35,"osprey,bat,cheetah","LIFT_BURST_POWER,MISSION_MULTI_GAIT,PAYLOAD_DAMPED,PAYLOAD_SLING_LOAD,STAB_COMPLIANT_SPINE,STAB_GUST_REJECTION,STRUCT_TENDON_CABLES,WING_FOLDABLE,WING_MORPHING_MEMBRANE",3,9,22.167099046814982,76.23491886253943,24,2.490116217344939,1.2857061336697877,12.018640701293577,0.0,li_ion,"Conventional high-TRL Li-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,8.850181918420262,215.20795366238815,1904.629540203093,2.167296079092967,86.69184316371869,titanium_alloy,heavy_robust,0.005,carbon_composite,steel,0.7,0.601973767221505,1.2,1.0219534724060828,2.0048912930959046,16.79147835523026,3.536127637372483,5,98.40201790935441,3.439102189309387,True,True,True,3.439102189309387,"Bio-inspired by osprey, bat, cheetah, this design is a heavy-lift VTOL rotorcraft concept. It uses 24 rotors, has an empty mass of 22.2 kg, and is configured to carry a payload of 76.2 kg (3.44:1 payload-to-aircraft mass ratio). The primary energy system is li-ion with a battery pack of 8.9 kg (~1905 Wh usable). It also incorporates approximately 2.2 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses titanium alloy (heavy_robust), with carbon_composite rotor blades and steel landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; multiple flight modes (hover, heavy-load cruise, light-load return, etc.); damped payload mounting to reduce oscillations during flight; a sling-load style payload mount hanging beneath the airframe; a compliant spine-like frame that absorbs dynamic loads. In the synthetic DARPA Lift mission model, it cruises at about 16.8 m/s and climbs at roughly 3.5 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.44. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by osprey, bat, cheetah, with 24 evenly spaced rotors and a compact central fuselage. Sleek titanium alloy airframe, carbon composite rotor blades, and rugged steel landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_8f85e7d07d,golden_eagle,"LIFT_BURST_POWER,LIFT_HIGH_CONTINUOUS,PAYLOAD_CENTRAL_TALON",1,3,12.172417821566134,56.47228815551702,5,2.4281519957259743,1.7959500477703005,7.870292601627869,0.0,li_s,Experimental lithium-sulfur chemistry with very high energy density but lower maturity and stability.,very_high,medium,low,0.05,9.903990005991517,363.53628527575427,3600.459736186351,1.2068322319334999,48.27328927734,titanium_alloy,heavy_robust,0.005,carbon_composite,titanium,0.4122956443911421,0.0,0.6185323429626006,4.46788440684549,2.4486267687091243,8.107542624531712,3.3070011851409524,6,68.64470597708315,4.639364913638099,True,True,True,4.639364913638099,"Bio-inspired by golden_eagle, this design is a heavy-lift VTOL rotorcraft concept. It uses 5 rotors, has an empty mass of 12.2 kg, and is configured to carry a payload of 56.5 kg (4.64:1 payload-to-aircraft mass ratio). The primary energy system is li-s with a battery pack of 9.9 kg (~3600 Wh usable). It also incorporates approximately 1.2 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses titanium alloy (heavy_robust), with carbon_composite rotor blades and titanium landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; strong continuous lifting capacity for heavy payloads; a central, talon-like payload cradle aligned with the center of gravity. In the synthetic DARPA Lift mission model, it cruises at about 8.1 m/s and climbs at roughly 3.3 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 4.64. ",rotor_plus_pusher,multirotor,pusher_propeller,0.533810587673901,1.05,0.9,0.01,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by golden_eagle, with 5 evenly spaced rotors and a compact central fuselage. Sleek titanium alloy airframe, carbon composite rotor blades, and rugged titanium landing gear. Subtle external cues of a li-s energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_765af8814f,"golden_eagle,cheetah,albatross,dragonfly,osprey","LIFT_BURST_POWER,LIFT_ENERGY_DENSE,LIFT_HIGH_CONTINUOUS,MISSION_GLIDE_SEGMENTS,MISSION_MULTI_GAIT,PAYLOAD_CENTRAL_TALON,PAYLOAD_DAMPED,PAYLOAD_SLING_LOAD,STAB_COMPLIANT_SPINE,STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION,STRUCT_TENDON_CABLES,WING_HIGH_ASPECT",5,13,12.69298888553027,75.78079348062414,9,1.6147628889995365,1.5102321620781562,4.749383555371783,0.0,li_ion,"Conventional high-TRL Li-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,9.505005359932799,198.2723538522601,1884.5797860922248,1.5264746547319406,61.05898618927762,carbon_composite,light_stiff,0.01,aluminum,titanium,0.6932587339748584,0.26808563205717933,1.2,3.3831542430451345,2.2149703954959445,16.05729576991729,5.655790678084516,5,88.47378236615441,5.970287547246858,True,True,True,5.970287547246858,"Bio-inspired by golden_eagle, cheetah, albatross, dragonfly, osprey, this design is a heavy-lift VTOL rotorcraft concept. It uses 9 rotors, has an empty mass of 12.7 kg, and is configured to carry a payload of 75.8 kg (5.97:1 payload-to-aircraft mass ratio). The primary energy system is li-ion with a battery pack of 9.5 kg (~1885 Wh usable). It also incorporates approximately 1.5 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses carbon composite (light_stiff), with aluminum rotor blades and titanium landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; an emphasis on energy-dense storage for long-range flight; strong continuous lifting capacity for heavy payloads; mission planning that includes partial-power or glide segments to save energy; multiple flight modes (hover, heavy-load cruise, light-load return, etc.). In the synthetic DARPA Lift mission model, it cruises at about 16.1 m/s and climbs at roughly 5.7 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 5.97. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by golden_eagle, cheetah, albatross, dragonfly, osprey, with 9 evenly spaced rotors and a compact central fuselage. Sleek carbon composite airframe, aluminum rotor blades, and rugged titanium landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_19d636ebaa,albatross,"LIFT_ENERGY_DENSE,MISSION_GLIDE_SEGMENTS,WING_HIGH_ASPECT",1,3,18.76931499935907,69.07825518538966,4,2.4313863670008207,1.0,0.0,0.0,li_ion,"Conventional high-TRL Li-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,8.91573465158398,247.92047902231374,2210.393205656542,0.0,0.0,magnesium_alloy,very_light_fragile,0.04,carbon_composite,steel,0.42004558454814533,0.0,1.2380433152748465,0.6031878500682392,2.493918540215097,19.233049494002053,2.372106553432353,3,87.84757018474873,3.680382325500346,True,True,True,3.680382325500346,"Bio-inspired by albatross, this design is a heavy-lift VTOL rotorcraft concept. It uses 4 rotors, has an empty mass of 18.8 kg, and is configured to carry a payload of 69.1 kg (3.68:1 payload-to-aircraft mass ratio). The primary energy system is li-ion with a battery pack of 8.9 kg (~2210 Wh usable). The main load-bearing frame uses magnesium alloy (very_light_fragile), with carbon_composite rotor blades and steel landing gear. Key bio-inspired features include an emphasis on energy-dense storage for long-range flight; mission planning that includes partial-power or glide segments to save energy; long, high-aspect-ratio lifting surfaces for efficient cruise. In the synthetic DARPA Lift mission model, it cruises at about 19.2 m/s and climbs at roughly 2.4 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.68. ",rotor_plus_small_jet,multirotor,small_jet,0.2559277655476111,1.15,0.85,0.03,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by albatross, with 4 evenly spaced rotors and a compact central fuselage. Sleek magnesium alloy airframe, carbon composite rotor blades, and rugged steel landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_0e9c309e70,golden_eagle,"LIFT_BURST_POWER,LIFT_HIGH_CONTINUOUS,PAYLOAD_CENTRAL_TALON",1,3,13.970192213318953,70.58164528851546,23,1.1564617313521288,2.6718495019759727,8.572492201041463,0.0,li_ion,"Conventional high-TRL Li-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,5.233969105151296,208.45942044034268,1091.070166262498,1.5403790261361885,61.615161045447536,titanium_alloy,heavy_robust,0.005,carbon_composite,composite,0.37002108515380144,0.0,1.106588339670762,2.4992449114844635,1.9961568944174184,9.997052564431021,3.8481729955049557,3,84.55183750183441,5.052303090090921,True,True,True,5.052303090090921,"Bio-inspired by golden_eagle, this design is a heavy-lift VTOL rotorcraft concept. It uses 23 rotors, has an empty mass of 14.0 kg, and is configured to carry a payload of 70.6 kg (5.05:1 payload-to-aircraft mass ratio). The primary energy system is li-ion with a battery pack of 5.2 kg (~1091 Wh usable). It also incorporates approximately 1.5 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses titanium alloy (heavy_robust), with carbon_composite rotor blades and composite landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; strong continuous lifting capacity for heavy payloads; a central, talon-like payload cradle aligned with the center of gravity. In the synthetic DARPA Lift mission model, it cruises at about 10.0 m/s and climbs at roughly 3.8 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 5.05. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by golden_eagle, with 23 evenly spaced rotors and a compact central fuselage. Sleek titanium alloy airframe, carbon composite rotor blades, and rugged composite landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_a7cbe74c46,"albatross,dragonfly,tiger,bat,cheetah","LIFT_BURST_POWER,LIFT_ENERGY_DENSE,MISSION_GLIDE_SEGMENTS,MISSION_MULTI_GAIT,STAB_COMPLIANT_SPINE,STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION,STRUCT_ROBUST_GEAR,STRUCT_TENDON_CABLES,WING_FOLDABLE,WING_HIGH_ASPECT,WING_MORPHING_MEMBRANE",5,12,17.987886624501932,52.63164653177022,16,1.2921304239848908,1.3989156133331733,18.039092775824404,0.0,li_ion,"Conventional high-TRL Li-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,8.6767894994228,244.1734466216902,2118.641597684955,2.384538732905611,95.38154931622444,steel_truss,heavy_robust,0.01,glass_composite,steel,0.7,0.3392756398083558,1.8690155248975504,3.52306717526883,1.915143823707901,8.596317473957384,3.275510269317518,4,70.61953315627215,2.925949425324863,True,True,True,2.925949425324863,"Bio-inspired by albatross, dragonfly, tiger, bat, cheetah, this design is a heavy-lift VTOL rotorcraft concept. It uses 16 rotors, has an empty mass of 18.0 kg, and is configured to carry a payload of 52.6 kg (2.93:1 payload-to-aircraft mass ratio). The primary energy system is li-ion with a battery pack of 8.7 kg (~2119 Wh usable). It also incorporates approximately 2.4 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses steel truss (heavy_robust), with glass_composite rotor blades and steel landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; an emphasis on energy-dense storage for long-range flight; mission planning that includes partial-power or glide segments to save energy; multiple flight modes (hover, heavy-load cruise, light-load return, etc.); a compliant spine-like frame that absorbs dynamic loads. In the synthetic DARPA Lift mission model, it cruises at about 8.6 m/s and climbs at roughly 3.3 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 2.93. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by albatross, dragonfly, tiger, bat, cheetah, with 16 evenly spaced rotors and a compact central fuselage. Sleek steel truss airframe, glass composite rotor blades, and rugged steel landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_e27a18966f,"tiger,dragonfly,golden_eagle,albatross","LIFT_BURST_POWER,LIFT_ENERGY_DENSE,LIFT_HIGH_CONTINUOUS,MISSION_GLIDE_SEGMENTS,PAYLOAD_CENTRAL_TALON,STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION,STRUCT_ROBUST_GEAR,STRUCT_TENDON_CABLES,WING_HIGH_ASPECT",4,10,12.474546765001246,51.68503930403814,23,1.4063325183682083,2.052897028297022,3.011619438525124,0.0,fuel_cell_li_ion_hybrid,"Hybrid hydrogen fuel-cell plus Li-ion buffer pack, high effective energy but complex and less mature.",extreme,medium_low,medium_low,0.06,4.813179450169271,452.19581824767306,2176.4996198421786,2.1508128980724486,86.03251592289794,steel_truss,heavy_robust,0.01,glass_composite,titanium,0.3311059787390256,0.4106264225638466,1.875836221221678,5.00804108355661,3.2894426627374043,22.213389331831014,5.842235001103031,4,64.15958606903939,4.143239852933685,True,True,True,4.143239852933685,"Bio-inspired by tiger, dragonfly, golden_eagle, albatross, this design is a heavy-lift VTOL rotorcraft concept. It uses 23 rotors, has an empty mass of 12.5 kg, and is configured to carry a payload of 51.7 kg (4.14:1 payload-to-aircraft mass ratio). The primary energy system is fuel-cell-li-ion-hybrid with a battery pack of 4.8 kg (~2176 Wh usable). It also incorporates approximately 2.2 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses steel truss (heavy_robust), with glass_composite rotor blades and titanium landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; an emphasis on energy-dense storage for long-range flight; strong continuous lifting capacity for heavy payloads; mission planning that includes partial-power or glide segments to save energy; a central, talon-like payload cradle aligned with the center of gravity. In the synthetic DARPA Lift mission model, it cruises at about 22.2 m/s and climbs at roughly 5.8 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 4.14. ",rotor_plus_pusher,multirotor,pusher_propeller,0.4648558211195336,1.05,0.9,0.01,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by tiger, dragonfly, golden_eagle, albatross, with 23 evenly spaced rotors and a compact central fuselage. Sleek steel truss airframe, glass composite rotor blades, and rugged titanium landing gear. Subtle external cues of a fuel-cell-li-ion-hybrid energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_fc39ceefc9,cheetah,"LIFT_BURST_POWER,MISSION_MULTI_GAIT,STAB_COMPLIANT_SPINE,STRUCT_TENDON_CABLES",1,4,13.758042101857104,72.36029984305947,11,1.58553417455652,1.6390373582823188,13.81517509408626,0.0,fuel_cell_li_ion_hybrid,"Hybrid hydrogen fuel-cell plus Li-ion buffer pack, high effective energy but complex and less mature.",extreme,medium_low,medium_low,0.06,10.394956248854788,668.0098284456215,6943.932940497228,2.187857841401998,87.51431365607992,aluminum_lithium,medium_stiff,0.02,carbon_composite,titanium,0.7,0.2453368133281212,1.6805300091359905,3.021447557989389,0.5962949154665633,13.764402826515509,3.6786129167408292,4,86.11834194491657,5.259491089454658,True,True,True,5.259491089454658,"Bio-inspired by cheetah, this design is a heavy-lift VTOL rotorcraft concept. It uses 11 rotors, has an empty mass of 13.8 kg, and is configured to carry a payload of 72.4 kg (5.26:1 payload-to-aircraft mass ratio). The primary energy system is fuel-cell-li-ion-hybrid with a battery pack of 10.4 kg (~6944 Wh usable). It also incorporates approximately 2.2 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses aluminum lithium (medium_stiff), with carbon_composite rotor blades and titanium landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; multiple flight modes (hover, heavy-load cruise, light-load return, etc.); a compliant spine-like frame that absorbs dynamic loads; a tendon/cable-based structural system to save mass in tension members. In the synthetic DARPA Lift mission model, it cruises at about 13.8 m/s and climbs at roughly 3.7 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 5.26. ",rotor_plus_small_jet,multirotor,small_jet,0.2479245980421543,1.15,0.85,0.03,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by cheetah, with 11 evenly spaced rotors and a compact central fuselage. Sleek aluminum lithium airframe, carbon composite rotor blades, and rugged titanium landing gear. Subtle external cues of a fuel-cell-li-ion-hybrid energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_8a38ce8405,"golden_eagle,harpy_eagle","LIFT_BURST_POWER,LIFT_HIGH_CONTINUOUS,PAYLOAD_CENTRAL_TALON",2,3,16.911277682685274,66.48987900611486,19,1.315025908323428,1.7216578424545461,10.26930127657713,0.0,li_ion,"Conventional high-TRL Li-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,8.958182034088809,228.01724224110148,2042.6199629067112,0.599024402282839,23.96097609131356,carbon_composite,light_stiff,0.01,carbon_composite,titanium,0.3930907929290041,0.0,1.765653611520405,1.4213132103708475,1.2949346970162459,14.781936242413146,4.64416021898402,2,83.40115668880014,3.9316886786260374,True,True,True,3.9316886786260374,"Bio-inspired by golden_eagle, harpy_eagle, this design is a heavy-lift VTOL rotorcraft concept. It uses 19 rotors, has an empty mass of 16.9 kg, and is configured to carry a payload of 66.5 kg (3.93:1 payload-to-aircraft mass ratio). The primary energy system is li-ion with a battery pack of 9.0 kg (~2043 Wh usable). It also incorporates approximately 0.6 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses carbon composite (light_stiff), with carbon_composite rotor blades and titanium landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; strong continuous lifting capacity for heavy payloads; a central, talon-like payload cradle aligned with the center of gravity. In the synthetic DARPA Lift mission model, it cruises at about 14.8 m/s and climbs at roughly 4.6 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.93. ",rotor_plus_pusher,multirotor,pusher_propeller,0.3550108468081987,1.05,0.9,0.01,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by golden_eagle, harpy_eagle, with 19 evenly spaced rotors and a compact central fuselage. Sleek carbon composite airframe, carbon composite rotor blades, and rugged titanium landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_d6adfb7d66,"golden_eagle,cheetah","LIFT_BURST_POWER,LIFT_HIGH_CONTINUOUS,MISSION_MULTI_GAIT,PAYLOAD_CENTRAL_TALON,STAB_COMPLIANT_SPINE,STRUCT_TENDON_CABLES",2,6,14.16098716008118,79.53103970747398,10,2.2318450098471083,1.2523719972770795,10.197373288365192,0.0,fuel_cell_li_ion_hybrid,"Hybrid hydrogen fuel-cell plus Li-ion buffer pack, high effective energy but complex and less mature.",extreme,medium_low,medium_low,0.06,6.918539209792565,798.9076907115102,5527.274183192414,1.8816786366971936,75.26714546788774,steel_truss,heavy_robust,0.01,carbon_composite,composite,0.7,0.04690836713402868,1.0821487295221262,2.4579652243245134,1.152253610739472,10.524016398144987,3.8326287244904607,4,93.69202686755516,5.616207317217711,True,True,True,5.616207317217711,"Bio-inspired by golden_eagle, cheetah, this design is a heavy-lift VTOL rotorcraft concept. It uses 10 rotors, has an empty mass of 14.2 kg, and is configured to carry a payload of 79.5 kg (5.62:1 payload-to-aircraft mass ratio). The primary energy system is fuel-cell-li-ion-hybrid with a battery pack of 6.9 kg (~5527 Wh usable). It also incorporates approximately 1.9 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses steel truss (heavy_robust), with carbon_composite rotor blades and composite landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; strong continuous lifting capacity for heavy payloads; multiple flight modes (hover, heavy-load cruise, light-load return, etc.); a central, talon-like payload cradle aligned with the center of gravity; a compliant spine-like frame that absorbs dynamic loads. In the synthetic DARPA Lift mission model, it cruises at about 10.5 m/s and climbs at roughly 3.8 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 5.62. ",rotor_plus_small_jet,multirotor,small_jet,0.28691737857664246,1.15,0.85,0.03,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by golden_eagle, cheetah, with 10 evenly spaced rotors and a compact central fuselage. Sleek steel truss airframe, carbon composite rotor blades, and rugged composite landing gear. Subtle external cues of a fuel-cell-li-ion-hybrid energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_acb07f4670,"golden_eagle,albatross,tiger,osprey","LIFT_BURST_POWER,LIFT_ENERGY_DENSE,LIFT_HIGH_CONTINUOUS,MISSION_GLIDE_SEGMENTS,PAYLOAD_CENTRAL_TALON,PAYLOAD_DAMPED,PAYLOAD_SLING_LOAD,STAB_GUST_REJECTION,STRUCT_ROBUST_GEAR,STRUCT_TENDON_CABLES,WING_HIGH_ASPECT",4,11,24.17774280754138,63.29331839994286,14,1.4771879734122693,1.8335454554107655,13.974431794269952,0.0,li_ion,"Conventional high-TRL Li-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,4.902514518953078,245.91755474041125,1205.6143825803044,2.2228343967600237,88.91337587040096,magnesium_alloy,very_light_fragile,0.04,aluminum,composite,0.5946199126440208,0.1112807098473003,1.2,2.3192591325945027,1.1569494630511794,22.025906819743845,5.517330365439424,2,87.47106120748424,2.617834051084404,True,True,True,2.617834051084404,"Bio-inspired by golden_eagle, albatross, tiger, osprey, this design is a heavy-lift VTOL rotorcraft concept. It uses 14 rotors, has an empty mass of 24.2 kg, and is configured to carry a payload of 63.3 kg (2.62:1 payload-to-aircraft mass ratio). The primary energy system is li-ion with a battery pack of 4.9 kg (~1206 Wh usable). It also incorporates approximately 2.2 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses magnesium alloy (very_light_fragile), with aluminum rotor blades and composite landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; an emphasis on energy-dense storage for long-range flight; strong continuous lifting capacity for heavy payloads; mission planning that includes partial-power or glide segments to save energy; a central, talon-like payload cradle aligned with the center of gravity. In the synthetic DARPA Lift mission model, it cruises at about 22.0 m/s and climbs at roughly 5.5 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 2.62. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by golden_eagle, albatross, tiger, osprey, with 14 evenly spaced rotors and a compact central fuselage. Sleek magnesium alloy airframe, aluminum rotor blades, and rugged composite landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_5733b51ed4,cheetah,"LIFT_BURST_POWER,MISSION_MULTI_GAIT,STAB_COMPLIANT_SPINE,STRUCT_TENDON_CABLES",1,4,23.393942975654646,69.42114662525073,23,2.221210731654236,1.4475400634466176,13.341846009242941,0.0,fuel_cell_li_ion_hybrid,"Hybrid hydrogen fuel-cell plus Li-ion buffer pack, high effective energy but complex and less mature.",extreme,medium_low,medium_low,0.06,9.414664392942338,683.7472785792957,6437.251157411721,0.8261356746511188,33.04542698604475,steel_truss,heavy_robust,0.01,aluminum,steel,0.4753836547436046,0.21150156389204636,1.2809568474923538,3.487407737650305,1.6689743116842524,5.146951453613298,5.997717519472701,4,92.81508960090537,2.967483792599442,True,True,True,2.967483792599442,"Bio-inspired by cheetah, this design is a heavy-lift VTOL rotorcraft concept. It uses 23 rotors, has an empty mass of 23.4 kg, and is configured to carry a payload of 69.4 kg (2.97:1 payload-to-aircraft mass ratio). The primary energy system is fuel-cell-li-ion-hybrid with a battery pack of 9.4 kg (~6437 Wh usable). It also incorporates approximately 0.8 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses steel truss (heavy_robust), with aluminum rotor blades and steel landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; multiple flight modes (hover, heavy-load cruise, light-load return, etc.); a compliant spine-like frame that absorbs dynamic loads; a tendon/cable-based structural system to save mass in tension members. In the synthetic DARPA Lift mission model, it cruises at about 5.1 m/s and climbs at roughly 6.0 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 2.97. ",rotor_plus_pusher,multirotor,pusher_propeller,0.437509017017633,1.05,0.9,0.01,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by cheetah, with 23 evenly spaced rotors and a compact central fuselage. Sleek steel truss airframe, aluminum rotor blades, and rugged steel landing gear. Subtle external cues of a fuel-cell-li-ion-hybrid energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_84a6d8e0c2,"tiger,dragonfly,bat","LIFT_BURST_POWER,STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION,STRUCT_ROBUST_GEAR,STRUCT_TENDON_CABLES,WING_FOLDABLE,WING_MORPHING_MEMBRANE",3,7,14.124833300769206,69.7284405402455,21,1.3535902009256011,1.1952061276254187,5.175050374832907,0.0,li_ion,"Conventional high-TRL Li-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,10.275094822282231,241.0334574655442,2476.6416308009975,0.5492050710377852,21.968202841511406,titanium_alloy,heavy_robust,0.005,carbon_composite,titanium,0.6310031338764651,0.5209469505399656,1.2,4.6919758015103,1.7439514109123295,10.211184708114072,3.176204486601371,2,83.85327384101471,4.936585024082957,True,True,True,4.936585024082957,"Bio-inspired by tiger, dragonfly, bat, this design is a heavy-lift VTOL rotorcraft concept. It uses 21 rotors, has an empty mass of 14.1 kg, and is configured to carry a payload of 69.7 kg (4.94:1 payload-to-aircraft mass ratio). The primary energy system is li-ion with a battery pack of 10.3 kg (~2477 Wh usable). It also incorporates approximately 0.5 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses titanium alloy (heavy_robust), with carbon_composite rotor blades and titanium landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; many smaller rotors for fine-grained control and redundancy; enhanced gust rejection and stability control for windy conditions; reinforced landing gear designed to tolerate higher touchdown loads; a tendon/cable-based structural system to save mass in tension members. In the synthetic DARPA Lift mission model, it cruises at about 10.2 m/s and climbs at roughly 3.2 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 4.94. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by tiger, dragonfly, bat, with 21 evenly spaced rotors and a compact central fuselage. Sleek titanium alloy airframe, carbon composite rotor blades, and rugged titanium landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_1df79ce4bf,"bat,tiger,albatross,cheetah","LIFT_BURST_POWER,LIFT_ENERGY_DENSE,MISSION_GLIDE_SEGMENTS,MISSION_MULTI_GAIT,STAB_COMPLIANT_SPINE,STRUCT_ROBUST_GEAR,STRUCT_TENDON_CABLES,WING_FOLDABLE,WING_HIGH_ASPECT,WING_MORPHING_MEMBRANE",4,10,12.058364219751704,66.01347808526775,15,2.430096061674565,2.7840127843948173,15.866411545611077,0.0,li_ion,"Conventional high-TRL Li-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,3.1612451306785143,180.32990671794826,570.0670395278247,2.200809722739975,88.032388909599,carbon_composite,light_stiff,0.01,aluminum,titanium,0.40908533197145064,0.35233553507975846,0.9591726381371191,0.7867849449375991,0.8871550552145149,23.969267501060333,3.8237052478740186,6,78.07184230501946,5.47449694521062,True,True,True,5.47449694521062,"Bio-inspired by bat, tiger, albatross, cheetah, this design is a heavy-lift VTOL rotorcraft concept. It uses 15 rotors, has an empty mass of 12.1 kg, and is configured to carry a payload of 66.0 kg (5.47:1 payload-to-aircraft mass ratio). The primary energy system is li-ion with a battery pack of 3.2 kg (~570 Wh usable). It also incorporates approximately 2.2 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses carbon composite (light_stiff), with aluminum rotor blades and titanium landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; an emphasis on energy-dense storage for long-range flight; mission planning that includes partial-power or glide segments to save energy; multiple flight modes (hover, heavy-load cruise, light-load return, etc.); a compliant spine-like frame that absorbs dynamic loads. In the synthetic DARPA Lift mission model, it cruises at about 24.0 m/s and climbs at roughly 3.8 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 5.47. ",rotor_plus_pusher,multirotor,pusher_propeller,0.3351340604831732,1.05,0.9,0.01,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by bat, tiger, albatross, cheetah, with 15 evenly spaced rotors and a compact central fuselage. Sleek carbon composite airframe, aluminum rotor blades, and rugged titanium landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_361e13dd2b,dragonfly,"STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION",1,2,17.26089320533579,53.029395415443844,20,1.4779680093520648,1.0,0.0,0.0,li_ion,"Conventional high-TRL Li-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,4.2344717068182804,246.4522176376712,1043.5949426693398,0.0,0.0,carbon_composite,light_stiff,0.01,glass_composite,titanium,0.4177896655668709,0.0,1.2,1.0757369843747888,0.899498772292717,10.259878312274637,4.092584430370323,3,70.29028862077963,3.07222776855204,True,True,True,3.07222776855204,"Bio-inspired by dragonfly, this design is a heavy-lift VTOL rotorcraft concept. It uses 20 rotors, has an empty mass of 17.3 kg, and is configured to carry a payload of 53.0 kg (3.07:1 payload-to-aircraft mass ratio). The primary energy system is li-ion with a battery pack of 4.2 kg (~1044 Wh usable). The main load-bearing frame uses carbon composite (light_stiff), with glass_composite rotor blades and titanium landing gear. Key bio-inspired features include many smaller rotors for fine-grained control and redundancy; enhanced gust rejection and stability control for windy conditions. In the synthetic DARPA Lift mission model, it cruises at about 10.3 m/s and climbs at roughly 4.1 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.07. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by dragonfly, with 20 evenly spaced rotors and a compact central fuselage. Sleek carbon composite airframe, glass composite rotor blades, and rugged titanium landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_053b388f15,"bee,cheetah,dragonfly","LIFT_BURST_POWER,LIFT_UNSTEADY_AERO,MISSION_MULTI_GAIT,STAB_COMPLIANT_SPINE,STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION,STRUCT_TENDON_CABLES",3,7,15.353867482252003,71.99203836015269,15,2.240950005351095,1.3657388406072855,9.8132177427728,0.2405774825374385,li_ion,"Conventional high-TRL Li-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,6.471439407833828,248.0537262429267,1605.2646592685,2.3996972908468504,95.98789163387401,titanium_alloy,heavy_robust,0.005,glass_composite,titanium,0.7,0.04105247696562416,1.91370048199985,1.2694606694250925,1.332055433261793,16.81500605980677,5.209059136180384,5,87.34590584240469,4.688853700435441,True,True,True,4.688853700435441,"Bio-inspired by bee, cheetah, dragonfly, this design is a heavy-lift VTOL rotorcraft concept. It uses 15 rotors, has an empty mass of 15.4 kg, and is configured to carry a payload of 72.0 kg (4.69:1 payload-to-aircraft mass ratio). The primary energy system is li-ion with a battery pack of 6.5 kg (~1605 Wh usable). It also incorporates approximately 2.4 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses titanium alloy (heavy_robust), with glass_composite rotor blades and titanium landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; unsteady aerodynamics (insect-like vortex lift) for better hover and low-speed lift; multiple flight modes (hover, heavy-load cruise, light-load return, etc.); a compliant spine-like frame that absorbs dynamic loads; many smaller rotors for fine-grained control and redundancy. In the synthetic DARPA Lift mission model, it cruises at about 16.8 m/s and climbs at roughly 5.2 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 4.69. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by bee, cheetah, dragonfly, with 15 evenly spaced rotors and a compact central fuselage. Sleek titanium alloy airframe, glass composite rotor blades, and rugged titanium landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_5ba7bbffb3,"tiger,cheetah","LIFT_BURST_POWER,MISSION_MULTI_GAIT,STAB_COMPLIANT_SPINE,STRUCT_ROBUST_GEAR,STRUCT_TENDON_CABLES",2,5,22.648389393075828,76.08246903838304,6,2.152002001466655,1.6412676310672136,8.625212322864426,0.0,li_ion,"Conventional high-TRL Li-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,7.562363989683678,224.03964557845433,1694.269347983997,1.1359127775567095,45.43651110226838,steel_truss,heavy_robust,0.01,carbon_composite,steel,0.7,0.061613903191778424,1.24768421926053,2.5056959397207152,3.6920122168371083,19.904779293145687,2.07107651539574,5,98.73085843145887,3.3592882795296397,True,True,True,3.3592882795296397,"Bio-inspired by tiger, cheetah, this design is a heavy-lift VTOL rotorcraft concept. It uses 6 rotors, has an empty mass of 22.6 kg, and is configured to carry a payload of 76.1 kg (3.36:1 payload-to-aircraft mass ratio). The primary energy system is li-ion with a battery pack of 7.6 kg (~1694 Wh usable). It also incorporates approximately 1.1 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses steel truss (heavy_robust), with carbon_composite rotor blades and steel landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; multiple flight modes (hover, heavy-load cruise, light-load return, etc.); a compliant spine-like frame that absorbs dynamic loads; reinforced landing gear designed to tolerate higher touchdown loads; a tendon/cable-based structural system to save mass in tension members. In the synthetic DARPA Lift mission model, it cruises at about 19.9 m/s and climbs at roughly 2.1 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.36. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by tiger, cheetah, with 6 evenly spaced rotors and a compact central fuselage. Sleek steel truss airframe, carbon composite rotor blades, and rugged steel landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_739e042cbf,"golden_eagle,dragonfly,cheetah,tiger","LIFT_BURST_POWER,LIFT_HIGH_CONTINUOUS,MISSION_MULTI_GAIT,PAYLOAD_CENTRAL_TALON,STAB_COMPLIANT_SPINE,STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION,STRUCT_ROBUST_GEAR,STRUCT_TENDON_CABLES",4,9,14.344292506645042,77.90648777459435,16,1.4018253061165244,2.6491082874152125,6.239838988970178,0.0,li_ion,"Conventional high-TRL Li-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,9.814344076292464,183.7200289527336,1803.091577848541,1.8997214027672906,75.98885611069163,titanium_alloy,heavy_robust,0.005,carbon_composite,composite,0.7,0.41252131662766056,1.256296364232555,5.577827971235634,0.7630128830007687,19.72427860626155,4.212905315616974,5,92.2507802812394,5.431183708677435,True,True,True,5.431183708677435,"Bio-inspired by golden_eagle, dragonfly, cheetah, tiger, this design is a heavy-lift VTOL rotorcraft concept. It uses 16 rotors, has an empty mass of 14.3 kg, and is configured to carry a payload of 77.9 kg (5.43:1 payload-to-aircraft mass ratio). The primary energy system is li-ion with a battery pack of 9.8 kg (~1803 Wh usable). It also incorporates approximately 1.9 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses titanium alloy (heavy_robust), with carbon_composite rotor blades and composite landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; strong continuous lifting capacity for heavy payloads; multiple flight modes (hover, heavy-load cruise, light-load return, etc.); a central, talon-like payload cradle aligned with the center of gravity; a compliant spine-like frame that absorbs dynamic loads. In the synthetic DARPA Lift mission model, it cruises at about 19.7 m/s and climbs at roughly 4.2 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 5.43. ",rotor_plus_small_jet,multirotor,small_jet,0.24487958906077792,1.15,0.85,0.03,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by golden_eagle, dragonfly, cheetah, tiger, with 16 evenly spaced rotors and a compact central fuselage. Sleek titanium alloy airframe, carbon composite rotor blades, and rugged composite landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_5f4e816d03,"tiger,bee,cheetah,harpy_eagle,osprey","LIFT_BURST_POWER,LIFT_HIGH_CONTINUOUS,LIFT_UNSTEADY_AERO,MISSION_MULTI_GAIT,PAYLOAD_CENTRAL_TALON,PAYLOAD_DAMPED,PAYLOAD_SLING_LOAD,STAB_COMPLIANT_SPINE,STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION,STRUCT_ROBUST_GEAR,STRUCT_TENDON_CABLES",5,12,19.02850264314282,67.48418813287574,17,2.043940879754843,2.78773200275584,12.0763476629613,0.21936930873859875,li_ion,"Conventional high-TRL Li-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,3.1149346359414594,188.51763726787098,587.2201178115398,1.1426109406052538,45.70443762421015,carbon_composite,light_stiff,0.01,carbon_composite,titanium,0.7,0.6884726755368029,1.5250854929971807,1.0934993147318308,0.936098471818749,20.687148018947326,2.8160036132810693,6,86.51269077601856,3.546479163308974,True,True,True,3.546479163308974,"Bio-inspired by tiger, bee, cheetah, harpy_eagle, osprey, this design is a heavy-lift VTOL rotorcraft concept. It uses 17 rotors, has an empty mass of 19.0 kg, and is configured to carry a payload of 67.5 kg (3.55:1 payload-to-aircraft mass ratio). The primary energy system is li-ion with a battery pack of 3.1 kg (~587 Wh usable). It also incorporates approximately 1.1 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses carbon composite (light_stiff), with carbon_composite rotor blades and titanium landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; strong continuous lifting capacity for heavy payloads; unsteady aerodynamics (insect-like vortex lift) for better hover and low-speed lift; multiple flight modes (hover, heavy-load cruise, light-load return, etc.); a central, talon-like payload cradle aligned with the center of gravity. In the synthetic DARPA Lift mission model, it cruises at about 20.7 m/s and climbs at roughly 2.8 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.55. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by tiger, bee, cheetah, harpy_eagle, osprey, with 17 evenly spaced rotors and a compact central fuselage. Sleek carbon composite airframe, carbon composite rotor blades, and rugged titanium landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_49f40b6d7c,"dragonfly,cheetah","LIFT_BURST_POWER,MISSION_MULTI_GAIT,STAB_COMPLIANT_SPINE,STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION,STRUCT_TENDON_CABLES",2,6,14.21782373110329,70.47976555104606,9,2.4474653485664217,2.4701589720524377,5.029014791640414,0.0,li_ion,"Conventional high-TRL Li-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,5.512010216782894,201.13916762475165,1108.6811469428383,0.4827865492698411,19.311461970793644,steel_truss,heavy_robust,0.01,carbon_composite,steel,0.7,0.027958412525000895,1.8929423576887325,3.3658055106654183,2.047321899717776,17.507333251179556,5.3725599247780504,4,84.69758928214935,4.957141605072979,True,True,True,4.957141605072979,"Bio-inspired by dragonfly, cheetah, this design is a heavy-lift VTOL rotorcraft concept. It uses 9 rotors, has an empty mass of 14.2 kg, and is configured to carry a payload of 70.5 kg (4.96:1 payload-to-aircraft mass ratio). The primary energy system is li-ion with a battery pack of 5.5 kg (~1109 Wh usable). It also incorporates approximately 0.5 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses steel truss (heavy_robust), with carbon_composite rotor blades and steel landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; multiple flight modes (hover, heavy-load cruise, light-load return, etc.); a compliant spine-like frame that absorbs dynamic loads; many smaller rotors for fine-grained control and redundancy; enhanced gust rejection and stability control for windy conditions. In the synthetic DARPA Lift mission model, it cruises at about 17.5 m/s and climbs at roughly 5.4 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 4.96. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by dragonfly, cheetah, with 9 evenly spaced rotors and a compact central fuselage. Sleek steel truss airframe, carbon composite rotor blades, and rugged steel landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_3e021efb8b,"dragonfly,tiger,harpy_eagle,cheetah","LIFT_BURST_POWER,LIFT_HIGH_CONTINUOUS,MISSION_MULTI_GAIT,PAYLOAD_CENTRAL_TALON,STAB_COMPLIANT_SPINE,STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION,STRUCT_ROBUST_GEAR,STRUCT_TENDON_CABLES",4,9,22.276363302999577,61.248741264859376,20,1.723779656600405,1.0877033218210035,18.270787351399505,0.0,li_ion,"Conventional high-TRL Li-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,7.625052301146902,255.85694557187344,1950.9225915972313,0.5021844276404848,20.08737710561939,steel_truss,heavy_robust,0.01,carbon_composite,titanium,0.3631217892462341,0.46923458830013964,1.660373399553915,5.502631672190966,2.0226283558234215,7.078536183473403,4.1510168560966445,5,83.52510456785896,2.749494629431369,True,True,True,2.749494629431369,"Bio-inspired by dragonfly, tiger, harpy_eagle, cheetah, this design is a heavy-lift VTOL rotorcraft concept. It uses 20 rotors, has an empty mass of 22.3 kg, and is configured to carry a payload of 61.2 kg (2.75:1 payload-to-aircraft mass ratio). The primary energy system is li-ion with a battery pack of 7.6 kg (~1951 Wh usable). It also incorporates approximately 0.5 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses steel truss (heavy_robust), with carbon_composite rotor blades and titanium landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; strong continuous lifting capacity for heavy payloads; multiple flight modes (hover, heavy-load cruise, light-load return, etc.); a central, talon-like payload cradle aligned with the center of gravity; a compliant spine-like frame that absorbs dynamic loads. In the synthetic DARPA Lift mission model, it cruises at about 7.1 m/s and climbs at roughly 4.2 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 2.75. ",rotor_plus_pusher,multirotor,pusher_propeller,0.5759004446033253,1.05,0.9,0.01,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by dragonfly, tiger, harpy_eagle, cheetah, with 20 evenly spaced rotors and a compact central fuselage. Sleek steel truss airframe, carbon composite rotor blades, and rugged titanium landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_0ee4f84a83,"albatross,osprey,bee,tiger,dragonfly","LIFT_BURST_POWER,LIFT_ENERGY_DENSE,LIFT_UNSTEADY_AERO,MISSION_GLIDE_SEGMENTS,PAYLOAD_DAMPED,PAYLOAD_SLING_LOAD,STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION,STRUCT_ROBUST_GEAR,STRUCT_TENDON_CABLES,WING_HIGH_ASPECT",5,11,15.687230866414891,69.02137007059355,13,2.0482046637070876,2.8283378327692357,16.515291077951808,0.18233114415396118,li_ion,"Conventional high-TRL Li-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,11.545185931774615,224.28193502114232,2589.3766409572804,1.6652092369207856,66.60836947683143,carbon_composite,light_stiff,0.01,carbon_composite,steel,0.743607077386935,0.6628855724602102,1.2,3.368561097849959,3.4606391279236375,11.877032996972938,3.6506179841049917,6,84.70860093700844,4.399844093476229,True,True,True,4.399844093476229,"Bio-inspired by albatross, osprey, bee, tiger, dragonfly, this design is a heavy-lift VTOL rotorcraft concept. It uses 13 rotors, has an empty mass of 15.7 kg, and is configured to carry a payload of 69.0 kg (4.40:1 payload-to-aircraft mass ratio). The primary energy system is li-ion with a battery pack of 11.5 kg (~2589 Wh usable). It also incorporates approximately 1.7 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses carbon composite (light_stiff), with carbon_composite rotor blades and steel landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; an emphasis on energy-dense storage for long-range flight; unsteady aerodynamics (insect-like vortex lift) for better hover and low-speed lift; mission planning that includes partial-power or glide segments to save energy; damped payload mounting to reduce oscillations during flight. In the synthetic DARPA Lift mission model, it cruises at about 11.9 m/s and climbs at roughly 3.7 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 4.40. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by albatross, osprey, bee, tiger, dragonfly, with 13 evenly spaced rotors and a compact central fuselage. Sleek carbon composite airframe, carbon composite rotor blades, and rugged steel landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_f1e81f7bb0,"bat,dragonfly","STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION,WING_FOLDABLE,WING_MORPHING_MEMBRANE",2,4,22.50137573475819,54.02917497148667,14,2.329040161311146,1.0,0.0,0.0,li_ion,"Conventional high-TRL Li-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,6.22867441902237,204.43774371562682,1273.3761445641762,0.0,0.0,titanium_alloy,heavy_robust,0.005,carbon_composite,steel,1.0226433612472996,0.0,1.7880704830561989,1.1880070086080394,1.5772360741560447,10.264693011871666,5.545343328315582,2,76.53055070624487,2.40114985005237,True,True,True,2.40114985005237,"Bio-inspired by bat, dragonfly, this design is a heavy-lift VTOL rotorcraft concept. It uses 14 rotors, has an empty mass of 22.5 kg, and is configured to carry a payload of 54.0 kg (2.40:1 payload-to-aircraft mass ratio). The primary energy system is li-ion with a battery pack of 6.2 kg (~1273 Wh usable). The main load-bearing frame uses titanium alloy (heavy_robust), with carbon_composite rotor blades and steel landing gear. Key bio-inspired features include many smaller rotors for fine-grained control and redundancy; enhanced gust rejection and stability control for windy conditions; foldable wings that deploy after vertical takeoff for cruise efficiency; morphing membrane-like lifting surfaces that can change area and camber. In the synthetic DARPA Lift mission model, it cruises at about 10.3 m/s and climbs at roughly 5.5 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 2.40. ",rotor_plus_pusher,multirotor,pusher_propeller,0.5568420738537021,1.05,0.9,0.01,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by bat, dragonfly, with 14 evenly spaced rotors and a compact central fuselage. Sleek titanium alloy airframe, carbon composite rotor blades, and rugged steel landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_fa090de0ac,"harpy_eagle,albatross,bat","LIFT_BURST_POWER,LIFT_ENERGY_DENSE,LIFT_HIGH_CONTINUOUS,MISSION_GLIDE_SEGMENTS,PAYLOAD_CENTRAL_TALON,WING_FOLDABLE,WING_HIGH_ASPECT,WING_MORPHING_MEMBRANE",3,8,18.0955268546706,51.88583484240407,15,1.4276261363918468,2.3371712000187346,11.804048906500215,0.0,li_s,Experimental lithium-sulfur chemistry with very high energy density but lower maturity and stability.,very_high,medium,low,0.05,6.492837989531964,437.68529160467176,2841.819688790188,2.6446559439548283,105.78623775819312,carbon_composite,light_stiff,0.01,glass_composite,titanium,1.0756998786438787,0.0,1.4503504726623797,1.311510243116674,1.9838194141286025,16.57262869840116,4.280640607292945,5,69.98136169707468,2.8673293272481826,True,True,True,2.8673293272481826,"Bio-inspired by harpy_eagle, albatross, bat, this design is a heavy-lift VTOL rotorcraft concept. It uses 15 rotors, has an empty mass of 18.1 kg, and is configured to carry a payload of 51.9 kg (2.87:1 payload-to-aircraft mass ratio). The primary energy system is li-s with a battery pack of 6.5 kg (~2842 Wh usable). It also incorporates approximately 2.6 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses carbon composite (light_stiff), with glass_composite rotor blades and titanium landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; an emphasis on energy-dense storage for long-range flight; strong continuous lifting capacity for heavy payloads; mission planning that includes partial-power or glide segments to save energy; a central, talon-like payload cradle aligned with the center of gravity. In the synthetic DARPA Lift mission model, it cruises at about 16.6 m/s and climbs at roughly 4.3 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 2.87. ",rotor_plus_pusher,multirotor,pusher_propeller,0.34611871119641907,1.05,0.9,0.01,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by harpy_eagle, albatross, bat, with 15 evenly spaced rotors and a compact central fuselage. Sleek carbon composite airframe, glass composite rotor blades, and rugged titanium landing gear. Subtle external cues of a li-s energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_faed73558d,"osprey,harpy_eagle","LIFT_BURST_POWER,LIFT_HIGH_CONTINUOUS,PAYLOAD_CENTRAL_TALON,PAYLOAD_DAMPED,PAYLOAD_SLING_LOAD,STAB_GUST_REJECTION",2,6,23.134970893363402,54.405953002552394,9,1.461563504423392,1.3600750791525942,19.290051720237415,0.0,li_ion,"Conventional high-TRL Li-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,8.072442321021887,181.48960285097894,1465.0643508796968,2.158641898512266,86.34567594049065,titanium_alloy,heavy_robust,0.005,carbon_composite,titanium,0.7066087061036626,0.0,1.9891637355619682,4.242670075766797,0.8411335679793925,21.607271494085616,4.4033548576448,6,77.5409238959158,2.3516758786223293,True,True,True,2.3516758786223293,"Bio-inspired by osprey, harpy_eagle, this design is a heavy-lift VTOL rotorcraft concept. It uses 9 rotors, has an empty mass of 23.1 kg, and is configured to carry a payload of 54.4 kg (2.35:1 payload-to-aircraft mass ratio). The primary energy system is li-ion with a battery pack of 8.1 kg (~1465 Wh usable). It also incorporates approximately 2.2 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses titanium alloy (heavy_robust), with carbon_composite rotor blades and titanium landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; strong continuous lifting capacity for heavy payloads; a central, talon-like payload cradle aligned with the center of gravity; damped payload mounting to reduce oscillations during flight; a sling-load style payload mount hanging beneath the airframe. In the synthetic DARPA Lift mission model, it cruises at about 21.6 m/s and climbs at roughly 4.4 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 2.35. ",rotor_plus_small_jet,multirotor,small_jet,0.1545652455610299,1.15,0.85,0.03,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by osprey, harpy_eagle, with 9 evenly spaced rotors and a compact central fuselage. Sleek titanium alloy airframe, carbon composite rotor blades, and rugged titanium landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_1ca7078447,"cheetah,bat","LIFT_BURST_POWER,MISSION_MULTI_GAIT,STAB_COMPLIANT_SPINE,STRUCT_TENDON_CABLES,WING_FOLDABLE,WING_MORPHING_MEMBRANE",2,6,16.38147267224715,74.13863116682933,22,1.2368036716854958,1.2677662112492027,11.11140102907718,0.0,li_ion,"Conventional high-TRL Li-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,10.731479225712704,202.66133344071648,2174.8558896742843,2.6302989395796734,105.21195758318694,aluminum_lithium,medium_stiff,0.02,carbon_composite,composite,0.7,0.4045910020603123,0.6767429059717265,0.5251791835770352,1.8090922416063948,18.75533473555552,3.2636068585170825,4,90.52010383907648,4.525761062522303,True,True,True,4.525761062522303,"Bio-inspired by cheetah, bat, this design is a heavy-lift VTOL rotorcraft concept. It uses 22 rotors, has an empty mass of 16.4 kg, and is configured to carry a payload of 74.1 kg (4.53:1 payload-to-aircraft mass ratio). The primary energy system is li-ion with a battery pack of 10.7 kg (~2175 Wh usable). It also incorporates approximately 2.6 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses aluminum lithium (medium_stiff), with carbon_composite rotor blades and composite landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; multiple flight modes (hover, heavy-load cruise, light-load return, etc.); a compliant spine-like frame that absorbs dynamic loads; a tendon/cable-based structural system to save mass in tension members; foldable wings that deploy after vertical takeoff for cruise efficiency. In the synthetic DARPA Lift mission model, it cruises at about 18.8 m/s and climbs at roughly 3.3 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 4.53. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by cheetah, bat, with 22 evenly spaced rotors and a compact central fuselage. Sleek aluminum lithium airframe, carbon composite rotor blades, and rugged composite landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_4246503186,golden_eagle,"LIFT_BURST_POWER,LIFT_HIGH_CONTINUOUS,PAYLOAD_CENTRAL_TALON",1,3,22.290693318967563,64.1500598026503,23,1.7095284083738695,1.1281609127386212,6.770094158531704,0.0,li_ion,"Conventional high-TRL Li-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,3.3397980445657103,210.74608083408177,703.8493486695534,2.9533443018938197,118.13377207575279,titanium_alloy,heavy_robust,0.005,carbon_composite,composite,0.8259654138703474,0.0,1.9185737867684116,4.044960684598525,1.780582629060274,13.779440970824716,2.8068289712240584,6,86.44075312161786,2.877885352631173,True,True,True,2.877885352631173,"Bio-inspired by golden_eagle, this design is a heavy-lift VTOL rotorcraft concept. It uses 23 rotors, has an empty mass of 22.3 kg, and is configured to carry a payload of 64.2 kg (2.88:1 payload-to-aircraft mass ratio). The primary energy system is li-ion with a battery pack of 3.3 kg (~704 Wh usable). It also incorporates approximately 3.0 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses titanium alloy (heavy_robust), with carbon_composite rotor blades and composite landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; strong continuous lifting capacity for heavy payloads; a central, talon-like payload cradle aligned with the center of gravity. In the synthetic DARPA Lift mission model, it cruises at about 13.8 m/s and climbs at roughly 2.8 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 2.88. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by golden_eagle, with 23 evenly spaced rotors and a compact central fuselage. Sleek titanium alloy airframe, carbon composite rotor blades, and rugged composite landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_e86fd93b2f,"bee,golden_eagle,bat","LIFT_BURST_POWER,LIFT_HIGH_CONTINUOUS,LIFT_UNSTEADY_AERO,PAYLOAD_CENTRAL_TALON,STAB_DISTRIBUTED_THRUST,WING_FOLDABLE,WING_MORPHING_MEMBRANE",3,7,18.416083588889737,57.730801599349014,21,2.238406289448924,2.149787757547818,14.8012616450121,0.24151386390827648,li_ion,"Conventional high-TRL Li-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,9.929704734604503,240.5978628037338,2389.06573741796,2.8837161759048433,115.34864703619374,aluminum_lithium,medium_stiff,0.02,carbon_composite,steel,0.3191454882724517,0.0,0.6744024521613838,0.7364399123143875,1.767323595116377,24.88396066730951,4.7076519042604,3,76.14688518823876,3.1348034081566345,True,True,True,3.1348034081566345,"Bio-inspired by bee, golden_eagle, bat, this design is a heavy-lift VTOL rotorcraft concept. It uses 21 rotors, has an empty mass of 18.4 kg, and is configured to carry a payload of 57.7 kg (3.13:1 payload-to-aircraft mass ratio). The primary energy system is li-ion with a battery pack of 9.9 kg (~2389 Wh usable). It also incorporates approximately 2.9 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses aluminum lithium (medium_stiff), with carbon_composite rotor blades and steel landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; strong continuous lifting capacity for heavy payloads; unsteady aerodynamics (insect-like vortex lift) for better hover and low-speed lift; a central, talon-like payload cradle aligned with the center of gravity; many smaller rotors for fine-grained control and redundancy. In the synthetic DARPA Lift mission model, it cruises at about 24.9 m/s and climbs at roughly 4.7 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.13. ",rotor_plus_small_jet,multirotor,small_jet,0.2237277916568049,1.15,0.85,0.03,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by bee, golden_eagle, bat, with 21 evenly spaced rotors and a compact central fuselage. Sleek aluminum lithium airframe, carbon composite rotor blades, and rugged steel landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_f41300e554,cheetah,"LIFT_BURST_POWER,MISSION_MULTI_GAIT,STAB_COMPLIANT_SPINE,STRUCT_TENDON_CABLES",1,4,16.639956692295847,59.46250717915752,22,2.316276369874375,1.9816107032130934,19.734709605518425,0.0,fuel_cell_li_ion_hybrid,"Hybrid hydrogen fuel-cell plus Li-ion buffer pack, high effective energy but complex and less mature.",extreme,medium_low,medium_low,0.06,5.5223996086486835,488.8371132319253,2699.553882804936,1.7299955590422291,69.19982236168917,carbon_composite,light_stiff,0.01,glass_composite,steel,0.7,0.3517326484851708,1.0905753842785968,2.611966736570727,0.8496007242380981,24.530143904740836,4.792978272384558,5,76.10246387145337,3.5734772799431704,True,True,True,3.5734772799431704,"Bio-inspired by cheetah, this design is a heavy-lift VTOL rotorcraft concept. It uses 22 rotors, has an empty mass of 16.6 kg, and is configured to carry a payload of 59.5 kg (3.57:1 payload-to-aircraft mass ratio). The primary energy system is fuel-cell-li-ion-hybrid with a battery pack of 5.5 kg (~2700 Wh usable). It also incorporates approximately 1.7 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses carbon composite (light_stiff), with glass_composite rotor blades and steel landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; multiple flight modes (hover, heavy-load cruise, light-load return, etc.); a compliant spine-like frame that absorbs dynamic loads; a tendon/cable-based structural system to save mass in tension members. In the synthetic DARPA Lift mission model, it cruises at about 24.5 m/s and climbs at roughly 4.8 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.57. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by cheetah, with 22 evenly spaced rotors and a compact central fuselage. Sleek carbon composite airframe, glass composite rotor blades, and rugged steel landing gear. Subtle external cues of a fuel-cell-li-ion-hybrid energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_d5a48126d9,"bee,cheetah,osprey,bat,dragonfly","LIFT_BURST_POWER,LIFT_UNSTEADY_AERO,MISSION_MULTI_GAIT,PAYLOAD_DAMPED,PAYLOAD_SLING_LOAD,STAB_COMPLIANT_SPINE,STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION,STRUCT_TENDON_CABLES,WING_FOLDABLE,WING_MORPHING_MEMBRANE",5,11,22.731274780615653,51.43127912247223,7,2.066760446344902,1.1200727554480332,16.83490717651639,0.11913485608803426,li_ion,"Conventional high-TRL Li-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,7.048693371574126,206.77252308116502,1457.4761128658658,1.0828860631653647,43.31544252661459,titanium_alloy,heavy_robust,0.005,aluminum,titanium,0.36096744355907673,0.08486624245169261,1.8010528759612052,4.645089555855239,0.8979162212737464,16.517889149466974,4.596523807598301,4,74.16255390308788,2.2625778632675204,True,True,True,2.2625778632675204,"Bio-inspired by bee, cheetah, osprey, bat, dragonfly, this design is a heavy-lift VTOL rotorcraft concept. It uses 7 rotors, has an empty mass of 22.7 kg, and is configured to carry a payload of 51.4 kg (2.26:1 payload-to-aircraft mass ratio). The primary energy system is li-ion with a battery pack of 7.0 kg (~1457 Wh usable). It also incorporates approximately 1.1 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses titanium alloy (heavy_robust), with aluminum rotor blades and titanium landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; unsteady aerodynamics (insect-like vortex lift) for better hover and low-speed lift; multiple flight modes (hover, heavy-load cruise, light-load return, etc.); damped payload mounting to reduce oscillations during flight; a sling-load style payload mount hanging beneath the airframe. In the synthetic DARPA Lift mission model, it cruises at about 16.5 m/s and climbs at roughly 4.6 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 2.26. ",ducted_fans_hybrid,ducted_fan_array,none,0.0,0.95,1.05,0.015,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by bee, cheetah, osprey, bat, dragonfly, with 7 evenly spaced rotors and a compact central fuselage. Sleek titanium alloy airframe, aluminum rotor blades, and rugged titanium landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_11ea0f8e19,"golden_eagle,albatross,tiger","LIFT_BURST_POWER,LIFT_ENERGY_DENSE,LIFT_HIGH_CONTINUOUS,MISSION_GLIDE_SEGMENTS,PAYLOAD_CENTRAL_TALON,STRUCT_ROBUST_GEAR,STRUCT_TENDON_CABLES,WING_HIGH_ASPECT",3,8,16.963069791254522,52.866611569477406,19,1.8678072413456115,1.052729826732482,9.74921285292288,0.0,li_s,Experimental lithium-sulfur chemistry with very high energy density but lower maturity and stability.,very_high,medium,low,0.05,3.7492608125161797,339.36783963974807,1272.3785421895825,0.4658230860004856,18.632923440019425,titanium_alloy,heavy_robust,0.005,aluminum,titanium,0.5441541980487297,0.1989226960406623,1.4397210269392846,1.3816366375593938,3.265553336678624,5.571425860398258,4.654196541215218,4,69.82968136073193,3.116571011028517,True,True,True,3.116571011028517,"Bio-inspired by golden_eagle, albatross, tiger, this design is a heavy-lift VTOL rotorcraft concept. It uses 19 rotors, has an empty mass of 17.0 kg, and is configured to carry a payload of 52.9 kg (3.12:1 payload-to-aircraft mass ratio). The primary energy system is li-s with a battery pack of 3.7 kg (~1272 Wh usable). It also incorporates approximately 0.5 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses titanium alloy (heavy_robust), with aluminum rotor blades and titanium landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; an emphasis on energy-dense storage for long-range flight; strong continuous lifting capacity for heavy payloads; mission planning that includes partial-power or glide segments to save energy; a central, talon-like payload cradle aligned with the center of gravity. In the synthetic DARPA Lift mission model, it cruises at about 5.6 m/s and climbs at roughly 4.7 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.12. ",rotor_plus_small_jet,multirotor,small_jet,0.24015804300080584,1.15,0.85,0.03,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by golden_eagle, albatross, tiger, with 19 evenly spaced rotors and a compact central fuselage. Sleek titanium alloy airframe, aluminum rotor blades, and rugged titanium landing gear. Subtle external cues of a li-s energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_71623e60fd,"albatross,harpy_eagle,dragonfly","LIFT_BURST_POWER,LIFT_ENERGY_DENSE,LIFT_HIGH_CONTINUOUS,MISSION_GLIDE_SEGMENTS,PAYLOAD_CENTRAL_TALON,STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION,WING_HIGH_ASPECT",3,8,16.67054845658792,62.35207607198404,21,1.7119489129830368,1.4997922355423792,15.153945710741008,0.0,li_ion,"Conventional high-TRL Li-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,10.455841700771618,197.64739409862773,2066.569865265274,0.23762919952510397,9.50516798100416,titanium_alloy,heavy_robust,0.005,carbon_composite,composite,0.8386390570185914,0.0,1.5408868381899627,1.7418334901008217,1.7969140819151235,15.63888532054553,3.0752880994350873,3,79.02262452857195,3.740253431634611,True,True,True,3.740253431634611,"Bio-inspired by albatross, harpy_eagle, dragonfly, this design is a heavy-lift VTOL rotorcraft concept. It uses 21 rotors, has an empty mass of 16.7 kg, and is configured to carry a payload of 62.4 kg (3.74:1 payload-to-aircraft mass ratio). The primary energy system is li-ion with a battery pack of 10.5 kg (~2067 Wh usable). It also incorporates approximately 0.2 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses titanium alloy (heavy_robust), with carbon_composite rotor blades and composite landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; an emphasis on energy-dense storage for long-range flight; strong continuous lifting capacity for heavy payloads; mission planning that includes partial-power or glide segments to save energy; a central, talon-like payload cradle aligned with the center of gravity. In the synthetic DARPA Lift mission model, it cruises at about 15.6 m/s and climbs at roughly 3.1 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.74. ",rotor_plus_small_jet,multirotor,small_jet,0.15472215370079284,1.15,0.85,0.03,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by albatross, harpy_eagle, dragonfly, with 21 evenly spaced rotors and a compact central fuselage. Sleek titanium alloy airframe, carbon composite rotor blades, and rugged composite landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_35397e7f7b,golden_eagle,"LIFT_BURST_POWER,LIFT_HIGH_CONTINUOUS,PAYLOAD_CENTRAL_TALON",1,3,24.182481285943247,71.4404756387239,16,2.1797154662382683,1.88592188428584,15.539523213409646,0.0,li_ion,"Conventional high-TRL Li-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,7.147511717810518,241.67967742321508,1727.408326339096,1.5634173601718517,62.53669440687407,steel_truss,heavy_robust,0.01,carbon_composite,steel,0.5444003837042912,0.0,0.9845947827243593,3.5126973562946824,0.5843718311894621,23.748418472644676,4.083705011670038,4,95.62295692466714,2.954224373999648,True,True,True,2.954224373999648,"Bio-inspired by golden_eagle, this design is a heavy-lift VTOL rotorcraft concept. It uses 16 rotors, has an empty mass of 24.2 kg, and is configured to carry a payload of 71.4 kg (2.95:1 payload-to-aircraft mass ratio). The primary energy system is li-ion with a battery pack of 7.1 kg (~1727 Wh usable). It also incorporates approximately 1.6 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses steel truss (heavy_robust), with carbon_composite rotor blades and steel landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; strong continuous lifting capacity for heavy payloads; a central, talon-like payload cradle aligned with the center of gravity. In the synthetic DARPA Lift mission model, it cruises at about 23.7 m/s and climbs at roughly 4.1 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 2.95. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by golden_eagle, with 16 evenly spaced rotors and a compact central fuselage. Sleek steel truss airframe, carbon composite rotor blades, and rugged steel landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_f9a413b4ba,"harpy_eagle,bat","LIFT_BURST_POWER,LIFT_HIGH_CONTINUOUS,PAYLOAD_CENTRAL_TALON,WING_FOLDABLE,WING_MORPHING_MEMBRANE",2,5,16.477093715630392,54.041965212828565,5,1.7794229864275184,1.8750000083301184,8.010148139495247,0.0,li_ion,"Conventional high-TRL Li-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,4.707982525976863,194.9301383159283,917.7276849776434,1.0429940370547963,41.719761482191856,magnesium_alloy,very_light_fragile,0.04,carbon_composite,composite,0.8461186212461691,0.0,1.3317804652490848,0.6299078354994493,0.8100509561506539,10.913453224214695,3.053397075581728,4,70.51905892845896,3.279823866120494,True,True,True,3.279823866120494,"Bio-inspired by harpy_eagle, bat, this design is a heavy-lift VTOL rotorcraft concept. It uses 5 rotors, has an empty mass of 16.5 kg, and is configured to carry a payload of 54.0 kg (3.28:1 payload-to-aircraft mass ratio). The primary energy system is li-ion with a battery pack of 4.7 kg (~918 Wh usable). It also incorporates approximately 1.0 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses magnesium alloy (very_light_fragile), with carbon_composite rotor blades and composite landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; strong continuous lifting capacity for heavy payloads; a central, talon-like payload cradle aligned with the center of gravity; foldable wings that deploy after vertical takeoff for cruise efficiency; morphing membrane-like lifting surfaces that can change area and camber. In the synthetic DARPA Lift mission model, it cruises at about 10.9 m/s and climbs at roughly 3.1 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.28. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by harpy_eagle, bat, with 5 evenly spaced rotors and a compact central fuselage. Sleek magnesium alloy airframe, carbon composite rotor blades, and rugged composite landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_37af6bf2fc,albatross,"LIFT_ENERGY_DENSE,MISSION_GLIDE_SEGMENTS,WING_HIGH_ASPECT",1,3,20.196867023725574,77.85211158315107,6,1.7552828008042867,1.0,0.0,0.0,li_ion,"Conventional high-TRL Li-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,6.248334460125706,239.47819527282945,1496.3398599719333,0.0,0.0,steel_truss,heavy_robust,0.01,glass_composite,composite,0.35785051796866635,0.0,1.4253999881351251,3.0570447823775697,1.9686006765125412,21.689129964099013,2.3117414994419656,3,98.04897860687664,3.8546627797121693,True,True,True,3.8546627797121693,"Bio-inspired by albatross, this design is a heavy-lift VTOL rotorcraft concept. It uses 6 rotors, has an empty mass of 20.2 kg, and is configured to carry a payload of 77.9 kg (3.85:1 payload-to-aircraft mass ratio). The primary energy system is li-ion with a battery pack of 6.2 kg (~1496 Wh usable). The main load-bearing frame uses steel truss (heavy_robust), with glass_composite rotor blades and composite landing gear. Key bio-inspired features include an emphasis on energy-dense storage for long-range flight; mission planning that includes partial-power or glide segments to save energy; long, high-aspect-ratio lifting surfaces for efficient cruise. In the synthetic DARPA Lift mission model, it cruises at about 21.7 m/s and climbs at roughly 2.3 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.85. ",ducted_fans_hybrid,ducted_fan_array,none,0.0,0.95,1.05,0.015,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by albatross, with 6 evenly spaced rotors and a compact central fuselage. Sleek steel truss airframe, glass composite rotor blades, and rugged composite landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_b6bbc7efb3,"albatross,tiger,cheetah,dragonfly,osprey","LIFT_BURST_POWER,LIFT_ENERGY_DENSE,MISSION_GLIDE_SEGMENTS,MISSION_MULTI_GAIT,PAYLOAD_DAMPED,PAYLOAD_SLING_LOAD,STAB_COMPLIANT_SPINE,STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION,STRUCT_ROBUST_GEAR,STRUCT_TENDON_CABLES,WING_HIGH_ASPECT",5,12,16.50010681167727,63.57210422623898,16,1.100273878997852,1.0693258044564198,7.836196900367498,0.0,li_ion,"Conventional high-TRL Li-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,4.2157713840954605,251.22596460690596,1059.111232531573,0.019706486918045885,0.7882594767218354,steel_truss,heavy_robust,0.01,carbon_composite,titanium,0.7,0.6603435343712822,1.7335061871553636,5.798351973019546,2.2838144650233483,16.41336410133875,4.286447321019017,4,80.07221103791625,3.8528298605466262,True,True,True,3.8528298605466262,"Bio-inspired by albatross, tiger, cheetah, dragonfly, osprey, this design is a heavy-lift VTOL rotorcraft concept. It uses 16 rotors, has an empty mass of 16.5 kg, and is configured to carry a payload of 63.6 kg (3.85:1 payload-to-aircraft mass ratio). The primary energy system is li-ion with a battery pack of 4.2 kg (~1059 Wh usable). It also incorporates approximately 0.0 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses steel truss (heavy_robust), with carbon_composite rotor blades and titanium landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; an emphasis on energy-dense storage for long-range flight; mission planning that includes partial-power or glide segments to save energy; multiple flight modes (hover, heavy-load cruise, light-load return, etc.); damped payload mounting to reduce oscillations during flight. In the synthetic DARPA Lift mission model, it cruises at about 16.4 m/s and climbs at roughly 4.3 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.85. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by albatross, tiger, cheetah, dragonfly, osprey, with 16 evenly spaced rotors and a compact central fuselage. Sleek steel truss airframe, carbon composite rotor blades, and rugged titanium landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_9a034fcec1,"harpy_eagle,bat,tiger,osprey,dragonfly","LIFT_BURST_POWER,LIFT_HIGH_CONTINUOUS,PAYLOAD_CENTRAL_TALON,PAYLOAD_DAMPED,PAYLOAD_SLING_LOAD,STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION,STRUCT_ROBUST_GEAR,STRUCT_TENDON_CABLES,WING_FOLDABLE,WING_MORPHING_MEMBRANE",5,11,12.51477815204454,66.19789188316008,8,1.5575642787170578,2.395537305188137,5.6043572042795775,0.0,li_ion,"Conventional high-TRL Li-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,11.976305727183403,257.6832195792295,3086.0930184457848,2.258520609031592,90.34082436126369,titanium_alloy,heavy_robust,0.005,carbon_composite,steel,0.978026480283063,0.10360868046084287,1.2,3.1183074581627586,2.9859451141054425,15.963048100350989,3.050231906326979,5,78.71267003520462,5.289577735930167,True,True,True,5.289577735930167,"Bio-inspired by harpy_eagle, bat, tiger, osprey, dragonfly, this design is a heavy-lift VTOL rotorcraft concept. It uses 8 rotors, has an empty mass of 12.5 kg, and is configured to carry a payload of 66.2 kg (5.29:1 payload-to-aircraft mass ratio). The primary energy system is li-ion with a battery pack of 12.0 kg (~3086 Wh usable). It also incorporates approximately 2.3 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses titanium alloy (heavy_robust), with carbon_composite rotor blades and steel landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; strong continuous lifting capacity for heavy payloads; a central, talon-like payload cradle aligned with the center of gravity; damped payload mounting to reduce oscillations during flight; a sling-load style payload mount hanging beneath the airframe. In the synthetic DARPA Lift mission model, it cruises at about 16.0 m/s and climbs at roughly 3.1 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 5.29. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by harpy_eagle, bat, tiger, osprey, dragonfly, with 8 evenly spaced rotors and a compact central fuselage. Sleek titanium alloy airframe, carbon composite rotor blades, and rugged steel landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_50cef1ac0e,golden_eagle,"LIFT_BURST_POWER,LIFT_HIGH_CONTINUOUS,PAYLOAD_CENTRAL_TALON",1,3,21.24477037550304,57.29144929698279,23,2.3974215731527497,2.737504703289937,16.942277259309936,0.0,li_ion,"Conventional high-TRL Li-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,9.244157025505057,188.90223938531759,1746.2419633474217,1.3501847119150379,54.00738847660151,carbon_composite,light_stiff,0.01,carbon_composite,steel,0.48692704171498596,0.0,1.284898822199797,1.2647727107906355,1.4660526606893836,19.598471670195778,2.5653896836957673,2,78.53621967248583,2.6967318678597967,True,True,True,2.6967318678597967,"Bio-inspired by golden_eagle, this design is a heavy-lift VTOL rotorcraft concept. It uses 23 rotors, has an empty mass of 21.2 kg, and is configured to carry a payload of 57.3 kg (2.70:1 payload-to-aircraft mass ratio). The primary energy system is li-ion with a battery pack of 9.2 kg (~1746 Wh usable). It also incorporates approximately 1.4 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses carbon composite (light_stiff), with carbon_composite rotor blades and steel landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; strong continuous lifting capacity for heavy payloads; a central, talon-like payload cradle aligned with the center of gravity. In the synthetic DARPA Lift mission model, it cruises at about 19.6 m/s and climbs at roughly 2.6 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 2.70. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by golden_eagle, with 23 evenly spaced rotors and a compact central fuselage. Sleek carbon composite airframe, carbon composite rotor blades, and rugged steel landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_7a51a04deb,"bat,osprey,harpy_eagle,cheetah","LIFT_BURST_POWER,LIFT_HIGH_CONTINUOUS,MISSION_MULTI_GAIT,PAYLOAD_CENTRAL_TALON,PAYLOAD_DAMPED,PAYLOAD_SLING_LOAD,STAB_COMPLIANT_SPINE,STAB_GUST_REJECTION,STRUCT_TENDON_CABLES,WING_FOLDABLE,WING_MORPHING_MEMBRANE",4,11,20.553891941151868,60.661343997396,13,1.430686671990098,2.9564885344890923,11.521274840011674,0.0,solid_state,Solid-state battery with improved safety and energy density but still under active development.,high,medium,medium_low,0.03,8.632131273441868,339.08095467720443,2926.991313097621,2.6712062582362845,106.84825032945139,steel_truss,heavy_robust,0.01,carbon_composite,steel,0.5209424758017307,0.10619572653807924,1.8457629724537572,3.6390395032207374,0.6755900342746028,12.644142437088167,5.842422773778287,6,81.21523593854786,2.951331269575433,True,True,True,2.951331269575433,"Bio-inspired by bat, osprey, harpy_eagle, cheetah, this design is a heavy-lift VTOL rotorcraft concept. It uses 13 rotors, has an empty mass of 20.6 kg, and is configured to carry a payload of 60.7 kg (2.95:1 payload-to-aircraft mass ratio). The primary energy system is solid-state with a battery pack of 8.6 kg (~2927 Wh usable). It also incorporates approximately 2.7 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses steel truss (heavy_robust), with carbon_composite rotor blades and steel landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; strong continuous lifting capacity for heavy payloads; multiple flight modes (hover, heavy-load cruise, light-load return, etc.); a central, talon-like payload cradle aligned with the center of gravity; damped payload mounting to reduce oscillations during flight. In the synthetic DARPA Lift mission model, it cruises at about 12.6 m/s and climbs at roughly 5.8 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 2.95. ",rotor_plus_small_jet,multirotor,small_jet,0.3059569937603801,1.15,0.85,0.03,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by bat, osprey, harpy_eagle, cheetah, with 13 evenly spaced rotors and a compact central fuselage. Sleek steel truss airframe, carbon composite rotor blades, and rugged steel landing gear. Subtle external cues of a solid-state energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_bb484d4c74,"albatross,golden_eagle","LIFT_BURST_POWER,LIFT_ENERGY_DENSE,LIFT_HIGH_CONTINUOUS,MISSION_GLIDE_SEGMENTS,PAYLOAD_CENTRAL_TALON,WING_HIGH_ASPECT",2,6,13.644323504040623,50.785946643899564,23,1.9637251077116105,2.2112090225077132,13.410154364447987,0.0,li_ion,"Conventional high-TRL Li-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,5.078211398321397,182.0867594237693,924.6750571891913,0.23842629093247514,9.537051637299005,magnesium_alloy,very_light_fragile,0.04,carbon_composite,composite,0.5653210039330426,0.0,1.4743528296123376,0.9723300213745611,1.27492057519325,14.476938417183266,2.655145501889581,3,64.43027014794019,3.7221300586181383,True,True,True,3.7221300586181383,"Bio-inspired by albatross, golden_eagle, this design is a heavy-lift VTOL rotorcraft concept. It uses 23 rotors, has an empty mass of 13.6 kg, and is configured to carry a payload of 50.8 kg (3.72:1 payload-to-aircraft mass ratio). The primary energy system is li-ion with a battery pack of 5.1 kg (~925 Wh usable). It also incorporates approximately 0.2 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses magnesium alloy (very_light_fragile), with carbon_composite rotor blades and composite landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; an emphasis on energy-dense storage for long-range flight; strong continuous lifting capacity for heavy payloads; mission planning that includes partial-power or glide segments to save energy; a central, talon-like payload cradle aligned with the center of gravity. In the synthetic DARPA Lift mission model, it cruises at about 14.5 m/s and climbs at roughly 2.7 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.72. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by albatross, golden_eagle, with 23 evenly spaced rotors and a compact central fuselage. Sleek magnesium alloy airframe, carbon composite rotor blades, and rugged composite landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_fcbacdb5ac,"tiger,bat,bee,harpy_eagle,dragonfly","LIFT_BURST_POWER,LIFT_HIGH_CONTINUOUS,LIFT_UNSTEADY_AERO,PAYLOAD_CENTRAL_TALON,STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION,STRUCT_ROBUST_GEAR,STRUCT_TENDON_CABLES,WING_FOLDABLE,WING_MORPHING_MEMBRANE",5,10,16.84247314893889,72.95479617207837,5,1.3657904759619468,1.8791077494329196,18.034758792649363,0.19341925313253142,li_ion,"Conventional high-TRL Li-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,4.498379415289756,203.5535780269708,915.6612253051027,2.7570984599265453,110.28393839706182,titanium_alloy,heavy_robust,0.005,aluminum,steel,0.865111713883407,0.06330856536219083,1.2509866853785319,1.626047815120257,2.5063431621605705,22.88656036497863,4.185628418186505,5,89.79726932101727,4.331596406711486,True,True,True,4.331596406711486,"Bio-inspired by tiger, bat, bee, harpy_eagle, dragonfly, this design is a heavy-lift VTOL rotorcraft concept. It uses 5 rotors, has an empty mass of 16.8 kg, and is configured to carry a payload of 73.0 kg (4.33:1 payload-to-aircraft mass ratio). The primary energy system is li-ion with a battery pack of 4.5 kg (~916 Wh usable). It also incorporates approximately 2.8 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses titanium alloy (heavy_robust), with aluminum rotor blades and steel landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; strong continuous lifting capacity for heavy payloads; unsteady aerodynamics (insect-like vortex lift) for better hover and low-speed lift; a central, talon-like payload cradle aligned with the center of gravity; many smaller rotors for fine-grained control and redundancy. In the synthetic DARPA Lift mission model, it cruises at about 22.9 m/s and climbs at roughly 4.2 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 4.33. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by tiger, bat, bee, harpy_eagle, dragonfly, with 5 evenly spaced rotors and a compact central fuselage. Sleek titanium alloy airframe, aluminum rotor blades, and rugged steel landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_f37d0801ec,"cheetah,dragonfly,bee","LIFT_BURST_POWER,LIFT_UNSTEADY_AERO,MISSION_MULTI_GAIT,STAB_COMPLIANT_SPINE,STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION,STRUCT_TENDON_CABLES",3,7,14.258700329582576,76.95625740250297,10,1.104946058031801,2.5307916142510023,3.2075320020088927,0.12440690185019943,li_ion,"Conventional high-TRL Li-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,10.267091073481403,228.63871448201115,2347.4545045105197,1.4804003887894381,59.21601555157753,carbon_composite,light_stiff,0.01,glass_composite,steel,0.6702440283532574,0.42085159659438925,1.2,3.228828774572358,1.056225875314564,17.57270851098726,5.280485565222874,4,91.21495773208555,5.397143892760096,True,True,True,5.397143892760096,"Bio-inspired by cheetah, dragonfly, bee, this design is a heavy-lift VTOL rotorcraft concept. It uses 10 rotors, has an empty mass of 14.3 kg, and is configured to carry a payload of 77.0 kg (5.40:1 payload-to-aircraft mass ratio). The primary energy system is li-ion with a battery pack of 10.3 kg (~2347 Wh usable). It also incorporates approximately 1.5 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses carbon composite (light_stiff), with glass_composite rotor blades and steel landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; unsteady aerodynamics (insect-like vortex lift) for better hover and low-speed lift; multiple flight modes (hover, heavy-load cruise, light-load return, etc.); a compliant spine-like frame that absorbs dynamic loads; many smaller rotors for fine-grained control and redundancy. In the synthetic DARPA Lift mission model, it cruises at about 17.6 m/s and climbs at roughly 5.3 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 5.40. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by cheetah, dragonfly, bee, with 10 evenly spaced rotors and a compact central fuselage. Sleek carbon composite airframe, glass composite rotor blades, and rugged steel landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_4006734908,"golden_eagle,cheetah,bee,bat,dragonfly","LIFT_BURST_POWER,LIFT_HIGH_CONTINUOUS,LIFT_UNSTEADY_AERO,MISSION_MULTI_GAIT,PAYLOAD_CENTRAL_TALON,STAB_COMPLIANT_SPINE,STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION,STRUCT_TENDON_CABLES,WING_FOLDABLE,WING_MORPHING_MEMBRANE",5,11,23.67364593485229,79.58835327032334,13,1.6978750471203212,2.6955959397031153,7.414220667866251,0.14378567225304306,li_ion,"Conventional high-TRL Li-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,11.343948313351111,229.14319846787114,2599.388599775486,1.489190776341538,59.567631053661515,magnesium_alloy,very_light_fragile,0.04,carbon_composite,composite,0.7,0.16290514764197875,1.2,1.0008274251945555,0.7364142689702926,14.297712687471618,5.1869302129127295,4,103.26199920517563,3.361896747520142,True,True,True,3.361896747520142,"Bio-inspired by golden_eagle, cheetah, bee, bat, dragonfly, this design is a heavy-lift VTOL rotorcraft concept. It uses 13 rotors, has an empty mass of 23.7 kg, and is configured to carry a payload of 79.6 kg (3.36:1 payload-to-aircraft mass ratio). The primary energy system is li-ion with a battery pack of 11.3 kg (~2599 Wh usable). It also incorporates approximately 1.5 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses magnesium alloy (very_light_fragile), with carbon_composite rotor blades and composite landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; strong continuous lifting capacity for heavy payloads; unsteady aerodynamics (insect-like vortex lift) for better hover and low-speed lift; multiple flight modes (hover, heavy-load cruise, light-load return, etc.); a central, talon-like payload cradle aligned with the center of gravity. In the synthetic DARPA Lift mission model, it cruises at about 14.3 m/s and climbs at roughly 5.2 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.36. ",rotor_plus_small_jet,multirotor,small_jet,0.39969610217503926,1.15,0.85,0.03,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by golden_eagle, cheetah, bee, bat, dragonfly, with 13 evenly spaced rotors and a compact central fuselage. Sleek magnesium alloy airframe, carbon composite rotor blades, and rugged composite landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_3c6ac6c640,"bee,tiger","LIFT_BURST_POWER,LIFT_UNSTEADY_AERO,STAB_DISTRIBUTED_THRUST,STRUCT_ROBUST_GEAR,STRUCT_TENDON_CABLES",2,5,12.827663016469524,54.47914718399793,4,1.5748133851369193,1.7504815552608795,12.082643995589748,0.04149237195212699,li_ion,"Conventional high-TRL Li-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,4.686410191332748,189.34757105385881,887.3603866909057,2.3470318112866626,93.8812724514665,aluminum_lithium,medium_stiff,0.02,aluminum,composite,0.4900481916197292,0.06075844949437752,1.8155730989311887,2.1606510229260216,3.2383724067522603,11.052574100515226,4.100401678750464,3,67.30681020046745,4.247004860827087,True,True,True,4.247004860827087,"Bio-inspired by bee, tiger, this design is a heavy-lift VTOL rotorcraft concept. It uses 4 rotors, has an empty mass of 12.8 kg, and is configured to carry a payload of 54.5 kg (4.25:1 payload-to-aircraft mass ratio). The primary energy system is li-ion with a battery pack of 4.7 kg (~887 Wh usable). It also incorporates approximately 2.3 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses aluminum lithium (medium_stiff), with aluminum rotor blades and composite landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; unsteady aerodynamics (insect-like vortex lift) for better hover and low-speed lift; many smaller rotors for fine-grained control and redundancy; reinforced landing gear designed to tolerate higher touchdown loads; a tendon/cable-based structural system to save mass in tension members. In the synthetic DARPA Lift mission model, it cruises at about 11.1 m/s and climbs at roughly 4.1 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 4.25. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by bee, tiger, with 4 evenly spaced rotors and a compact central fuselage. Sleek aluminum lithium airframe, aluminum rotor blades, and rugged composite landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_559bfaf1d7,"harpy_eagle,dragonfly,bee","LIFT_BURST_POWER,LIFT_HIGH_CONTINUOUS,LIFT_UNSTEADY_AERO,PAYLOAD_CENTRAL_TALON,STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION",3,6,23.151694805346956,59.626411095385734,10,1.5011943279751343,2.0645516115300326,16.13738065584723,0.16778101048926047,li_ion,"Conventional high-TRL Li-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,4.417464133074372,189.15683151200813,835.593518730288,2.874894163525364,114.99576654101458,titanium_alloy,heavy_robust,0.005,carbon_composite,steel,0.7872393538533177,0.0,1.2,4.561766838716608,2.10800567691427,16.481658852819365,2.6850999018920323,4,82.7781059007327,2.5754663577205945,True,True,True,2.5754663577205945,"Bio-inspired by harpy_eagle, dragonfly, bee, this design is a heavy-lift VTOL rotorcraft concept. It uses 10 rotors, has an empty mass of 23.2 kg, and is configured to carry a payload of 59.6 kg (2.58:1 payload-to-aircraft mass ratio). The primary energy system is li-ion with a battery pack of 4.4 kg (~836 Wh usable). It also incorporates approximately 2.9 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses titanium alloy (heavy_robust), with carbon_composite rotor blades and steel landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; strong continuous lifting capacity for heavy payloads; unsteady aerodynamics (insect-like vortex lift) for better hover and low-speed lift; a central, talon-like payload cradle aligned with the center of gravity; many smaller rotors for fine-grained control and redundancy. In the synthetic DARPA Lift mission model, it cruises at about 16.5 m/s and climbs at roughly 2.7 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 2.58. ",rotor_plus_pusher,multirotor,pusher_propeller,0.3354955570118937,1.05,0.9,0.01,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by harpy_eagle, dragonfly, bee, with 10 evenly spaced rotors and a compact central fuselage. Sleek titanium alloy airframe, carbon composite rotor blades, and rugged steel landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_c23de94e79,"dragonfly,bee,albatross,golden_eagle,osprey","LIFT_BURST_POWER,LIFT_ENERGY_DENSE,LIFT_HIGH_CONTINUOUS,LIFT_UNSTEADY_AERO,MISSION_GLIDE_SEGMENTS,PAYLOAD_CENTRAL_TALON,PAYLOAD_DAMPED,PAYLOAD_SLING_LOAD,STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION,WING_HIGH_ASPECT",5,11,21.859733829348496,76.47211670683944,18,1.7825094255981577,1.13073039763174,4.919079974103673,0.11966302145503774,solid_state,Solid-state battery with improved safety and energy density but still under active development.,high,medium,medium_low,0.03,5.54031632029618,291.37538980245307,1614.3118274551919,1.7240347741706816,68.96139096682727,aluminum_lithium,medium_stiff,0.02,carbon_composite,composite,0.37488690635643007,0.0,1.334224790142306,0.7482339648418745,1.1042362530938619,14.219497054936955,4.36214382688528,3,98.33185053618794,3.498309599916963,True,True,True,3.498309599916963,"Bio-inspired by dragonfly, bee, albatross, golden_eagle, osprey, this design is a heavy-lift VTOL rotorcraft concept. It uses 18 rotors, has an empty mass of 21.9 kg, and is configured to carry a payload of 76.5 kg (3.50:1 payload-to-aircraft mass ratio). The primary energy system is solid-state with a battery pack of 5.5 kg (~1614 Wh usable). It also incorporates approximately 1.7 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses aluminum lithium (medium_stiff), with carbon_composite rotor blades and composite landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; an emphasis on energy-dense storage for long-range flight; strong continuous lifting capacity for heavy payloads; unsteady aerodynamics (insect-like vortex lift) for better hover and low-speed lift; mission planning that includes partial-power or glide segments to save energy. In the synthetic DARPA Lift mission model, it cruises at about 14.2 m/s and climbs at roughly 4.4 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.50. ",rotor_plus_pusher,multirotor,pusher_propeller,0.41917960691160044,1.05,0.9,0.01,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by dragonfly, bee, albatross, golden_eagle, osprey, with 18 evenly spaced rotors and a compact central fuselage. Sleek aluminum lithium airframe, carbon composite rotor blades, and rugged composite landing gear. Subtle external cues of a solid-state energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_da1306bc1f,osprey,"PAYLOAD_DAMPED,PAYLOAD_SLING_LOAD,STAB_GUST_REJECTION",1,3,20.261017422118822,63.589232608211596,13,1.6459757243231015,1.0,0.0,0.0,li_ion,"Conventional high-TRL Li-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,4.76099958159741,234.5213430389317,1116.5560160840164,0.0,0.0,aluminum_lithium,medium_stiff,0.02,carbon_composite,composite,0.5131850931268269,0.0,1.9149999462441705,2.0215446167608295,2.4651606070267844,11.885292528612801,2.357149618349283,2,83.85025003033041,3.1385014524883452,True,True,True,3.1385014524883452,"Bio-inspired by osprey, this design is a heavy-lift VTOL rotorcraft concept. It uses 13 rotors, has an empty mass of 20.3 kg, and is configured to carry a payload of 63.6 kg (3.14:1 payload-to-aircraft mass ratio). The primary energy system is li-ion with a battery pack of 4.8 kg (~1117 Wh usable). The main load-bearing frame uses aluminum lithium (medium_stiff), with carbon_composite rotor blades and composite landing gear. Key bio-inspired features include damped payload mounting to reduce oscillations during flight; a sling-load style payload mount hanging beneath the airframe; enhanced gust rejection and stability control for windy conditions. In the synthetic DARPA Lift mission model, it cruises at about 11.9 m/s and climbs at roughly 2.4 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.14. ",rotor_plus_pusher,multirotor,pusher_propeller,0.4041695517426652,1.05,0.9,0.01,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by osprey, with 13 evenly spaced rotors and a compact central fuselage. Sleek aluminum lithium airframe, carbon composite rotor blades, and rugged composite landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_4c79047177,"golden_eagle,osprey","LIFT_BURST_POWER,LIFT_HIGH_CONTINUOUS,PAYLOAD_CENTRAL_TALON,PAYLOAD_DAMPED,PAYLOAD_SLING_LOAD,STAB_GUST_REJECTION",2,6,20.028036244766938,62.47566398832636,18,2.3510154567994164,2.390781039065562,18.815287211812816,0.0,li_ion,"Conventional high-TRL Li-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,7.089549232905613,213.9299747658074,1516.667088496447,2.4602142747501827,98.4085709900073,aluminum_lithium,medium_stiff,0.02,carbon_composite,steel,0.3052009940486919,0.0,1.24723544545625,3.0581968302177254,1.9242599979300619,10.385008962577253,5.7062578066040945,6,82.5037002330933,3.1194103717807296,True,True,True,3.1194103717807296,"Bio-inspired by golden_eagle, osprey, this design is a heavy-lift VTOL rotorcraft concept. It uses 18 rotors, has an empty mass of 20.0 kg, and is configured to carry a payload of 62.5 kg (3.12:1 payload-to-aircraft mass ratio). The primary energy system is li-ion with a battery pack of 7.1 kg (~1517 Wh usable). It also incorporates approximately 2.5 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses aluminum lithium (medium_stiff), with carbon_composite rotor blades and steel landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; strong continuous lifting capacity for heavy payloads; a central, talon-like payload cradle aligned with the center of gravity; damped payload mounting to reduce oscillations during flight; a sling-load style payload mount hanging beneath the airframe. In the synthetic DARPA Lift mission model, it cruises at about 10.4 m/s and climbs at roughly 5.7 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.12. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by golden_eagle, osprey, with 18 evenly spaced rotors and a compact central fuselage. Sleek aluminum lithium airframe, carbon composite rotor blades, and rugged steel landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_8916b91234,"dragonfly,tiger,harpy_eagle,bee,albatross","LIFT_BURST_POWER,LIFT_ENERGY_DENSE,LIFT_HIGH_CONTINUOUS,LIFT_UNSTEADY_AERO,MISSION_GLIDE_SEGMENTS,PAYLOAD_CENTRAL_TALON,STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION,STRUCT_ROBUST_GEAR,STRUCT_TENDON_CABLES,WING_HIGH_ASPECT",5,11,19.226763588290588,67.18579986355152,13,2.2324540915513937,2.2486340109601333,7.875866124338828,0.02062754170377054,li_ion,"Conventional high-TRL Li-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,10.663007304473709,202.22790375474153,2156.357614905215,0.39761628841901775,15.90465153676071,carbon_composite,light_stiff,0.01,aluminum,titanium,0.4158930413048162,0.12222969336131244,1.387655188206217,1.1112926188976193,2.0899595030345055,21.15681382647147,3.0450103516139895,3,86.41256345184212,3.494389451195456,True,True,True,3.494389451195456,"Bio-inspired by dragonfly, tiger, harpy_eagle, bee, albatross, this design is a heavy-lift VTOL rotorcraft concept. It uses 13 rotors, has an empty mass of 19.2 kg, and is configured to carry a payload of 67.2 kg (3.49:1 payload-to-aircraft mass ratio). The primary energy system is li-ion with a battery pack of 10.7 kg (~2156 Wh usable). It also incorporates approximately 0.4 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses carbon composite (light_stiff), with aluminum rotor blades and titanium landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; an emphasis on energy-dense storage for long-range flight; strong continuous lifting capacity for heavy payloads; unsteady aerodynamics (insect-like vortex lift) for better hover and low-speed lift; mission planning that includes partial-power or glide segments to save energy. In the synthetic DARPA Lift mission model, it cruises at about 21.2 m/s and climbs at roughly 3.0 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.49. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by dragonfly, tiger, harpy_eagle, bee, albatross, with 13 evenly spaced rotors and a compact central fuselage. Sleek carbon composite airframe, aluminum rotor blades, and rugged titanium landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_a85c1fc478,dragonfly,"STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION",1,2,23.590281575667582,63.464618708641254,14,2.4464678119298426,1.0,0.0,0.0,li_ion,"Conventional high-TRL Li-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,3.36915853527396,253.41697128492197,853.8019517878708,0.0,0.0,titanium_alloy,heavy_robust,0.005,aluminum,steel,1.0840238232159096,0.0,1.7875335097974978,2.006863107795787,1.0341756314384394,6.965535768172728,4.617373126273657,5,87.05490028430884,2.690286612521931,True,True,True,2.690286612521931,"Bio-inspired by dragonfly, this design is a heavy-lift VTOL rotorcraft concept. It uses 14 rotors, has an empty mass of 23.6 kg, and is configured to carry a payload of 63.5 kg (2.69:1 payload-to-aircraft mass ratio). The primary energy system is li-ion with a battery pack of 3.4 kg (~854 Wh usable). The main load-bearing frame uses titanium alloy (heavy_robust), with aluminum rotor blades and steel landing gear. Key bio-inspired features include many smaller rotors for fine-grained control and redundancy; enhanced gust rejection and stability control for windy conditions. In the synthetic DARPA Lift mission model, it cruises at about 7.0 m/s and climbs at roughly 4.6 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 2.69. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by dragonfly, with 14 evenly spaced rotors and a compact central fuselage. Sleek titanium alloy airframe, aluminum rotor blades, and rugged steel landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_90739f8c70,"golden_eagle,osprey","LIFT_BURST_POWER,LIFT_HIGH_CONTINUOUS,PAYLOAD_CENTRAL_TALON,PAYLOAD_DAMPED,PAYLOAD_SLING_LOAD,STAB_GUST_REJECTION",2,6,15.166696736083237,64.00866731862973,6,1.9942927109809312,2.845390781689396,7.6985205566816415,0.0,li_ion,"Conventional high-TRL Li-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,11.130523435832655,241.59044073231198,2689.0280624441384,0.9702123833597434,38.80849533438973,carbon_composite,light_stiff,0.01,carbon_composite,composite,0.6247552318812506,0.0,1.2,0.6391847406584887,2.4112113984346517,10.293297049094658,3.7622993311106705,5,79.17536405471297,4.220343324090214,True,True,True,4.220343324090214,"Bio-inspired by golden_eagle, osprey, this design is a heavy-lift VTOL rotorcraft concept. It uses 6 rotors, has an empty mass of 15.2 kg, and is configured to carry a payload of 64.0 kg (4.22:1 payload-to-aircraft mass ratio). The primary energy system is li-ion with a battery pack of 11.1 kg (~2689 Wh usable). It also incorporates approximately 1.0 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses carbon composite (light_stiff), with carbon_composite rotor blades and composite landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; strong continuous lifting capacity for heavy payloads; a central, talon-like payload cradle aligned with the center of gravity; damped payload mounting to reduce oscillations during flight; a sling-load style payload mount hanging beneath the airframe. In the synthetic DARPA Lift mission model, it cruises at about 10.3 m/s and climbs at roughly 3.8 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 4.22. ",ducted_fans_hybrid,ducted_fan_array,none,0.0,0.95,1.05,0.015,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by golden_eagle, osprey, with 6 evenly spaced rotors and a compact central fuselage. Sleek carbon composite airframe, carbon composite rotor blades, and rugged composite landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_0ef9d5711d,"cheetah,golden_eagle,dragonfly,bat","LIFT_BURST_POWER,LIFT_HIGH_CONTINUOUS,MISSION_MULTI_GAIT,PAYLOAD_CENTRAL_TALON,STAB_COMPLIANT_SPINE,STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION,STRUCT_TENDON_CABLES,WING_FOLDABLE,WING_MORPHING_MEMBRANE",4,10,23.688027343861886,60.767549797916345,13,1.6608607178723256,2.2645450531991687,19.300006076695507,0.0,li_ion,"Conventional high-TRL Li-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,7.811636669040312,256.87404176000524,2006.6066839370494,0.24137035402316398,9.65481416092656,aluminum_lithium,medium_stiff,0.02,glass_composite,steel,0.42363281315664075,0.027531827816807217,1.2,1.1685110632035598,1.8917645572141515,22.929213957006933,4.522468229795772,4,84.45557714177824,2.5653275773367685,True,True,True,2.5653275773367685,"Bio-inspired by cheetah, golden_eagle, dragonfly, bat, this design is a heavy-lift VTOL rotorcraft concept. It uses 13 rotors, has an empty mass of 23.7 kg, and is configured to carry a payload of 60.8 kg (2.57:1 payload-to-aircraft mass ratio). The primary energy system is li-ion with a battery pack of 7.8 kg (~2007 Wh usable). It also incorporates approximately 0.2 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses aluminum lithium (medium_stiff), with glass_composite rotor blades and steel landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; strong continuous lifting capacity for heavy payloads; multiple flight modes (hover, heavy-load cruise, light-load return, etc.); a central, talon-like payload cradle aligned with the center of gravity; a compliant spine-like frame that absorbs dynamic loads. In the synthetic DARPA Lift mission model, it cruises at about 22.9 m/s and climbs at roughly 4.5 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 2.57. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by cheetah, golden_eagle, dragonfly, bat, with 13 evenly spaced rotors and a compact central fuselage. Sleek aluminum lithium airframe, glass composite rotor blades, and rugged steel landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_f0ab2caaf0,osprey,"PAYLOAD_DAMPED,PAYLOAD_SLING_LOAD,STAB_GUST_REJECTION",1,3,19.908268184397183,77.13987051859587,7,1.7386584300973733,1.0,0.0,0.0,li_ion,"Conventional high-TRL Li-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,8.319382403609293,245.42401422111413,2041.7762253342937,0.0,0.0,carbon_composite,light_stiff,0.01,carbon_composite,composite,0.49984084366705106,0.0,1.7066802963909633,1.792566111405423,2.1230420594795936,24.643855055857955,4.713591349184769,4,97.04813870299306,3.874765489599599,True,True,True,3.874765489599599,"Bio-inspired by osprey, this design is a heavy-lift VTOL rotorcraft concept. It uses 7 rotors, has an empty mass of 19.9 kg, and is configured to carry a payload of 77.1 kg (3.87:1 payload-to-aircraft mass ratio). The primary energy system is li-ion with a battery pack of 8.3 kg (~2042 Wh usable). The main load-bearing frame uses carbon composite (light_stiff), with carbon_composite rotor blades and composite landing gear. Key bio-inspired features include damped payload mounting to reduce oscillations during flight; a sling-load style payload mount hanging beneath the airframe; enhanced gust rejection and stability control for windy conditions. In the synthetic DARPA Lift mission model, it cruises at about 24.6 m/s and climbs at roughly 4.7 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.87. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by osprey, with 7 evenly spaced rotors and a compact central fuselage. Sleek carbon composite airframe, carbon composite rotor blades, and rugged composite landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_5136c5a0fb,"bat,albatross,golden_eagle,dragonfly","LIFT_BURST_POWER,LIFT_ENERGY_DENSE,LIFT_HIGH_CONTINUOUS,MISSION_GLIDE_SEGMENTS,PAYLOAD_CENTRAL_TALON,STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION,WING_FOLDABLE,WING_HIGH_ASPECT,WING_MORPHING_MEMBRANE",4,10,20.64591962076921,67.88815912157307,19,1.956869744736085,1.1760423872946448,17.050221169769102,0.0,li_ion,"Conventional high-TRL Li-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,6.769072830983477,224.61683227755964,1520.4476967516014,0.5757085856238264,23.028343424953057,steel_truss,heavy_robust,0.01,aluminum,steel,0.9491073291706237,0.0,1.980173184049012,2.959310442564684,1.428432014142443,17.529284903306834,2.832434811485606,2,88.53407874234227,3.2882119260640494,True,True,True,3.2882119260640494,"Bio-inspired by bat, albatross, golden_eagle, dragonfly, this design is a heavy-lift VTOL rotorcraft concept. It uses 19 rotors, has an empty mass of 20.6 kg, and is configured to carry a payload of 67.9 kg (3.29:1 payload-to-aircraft mass ratio). The primary energy system is li-ion with a battery pack of 6.8 kg (~1520 Wh usable). It also incorporates approximately 0.6 kg of high-power supercapacitors to support short burst power for takeoff and climb. The main load-bearing frame uses steel truss (heavy_robust), with aluminum rotor blades and steel landing gear. Key bio-inspired features include short burst thrust for takeoff and climb via high-power propulsion or supercapacitors; an emphasis on energy-dense storage for long-range flight; strong continuous lifting capacity for heavy payloads; mission planning that includes partial-power or glide segments to save energy; a central, talon-like payload cradle aligned with the center of gravity. In the synthetic DARPA Lift mission model, it cruises at about 17.5 m/s and climbs at roughly 2.8 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.29. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by bat, albatross, golden_eagle, dragonfly, with 19 evenly spaced rotors and a compact central fuselage. Sleek steel truss airframe, aluminum rotor blades, and rugged steel landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."
DLIFT_ad26106076,"bat,albatross","LIFT_ENERGY_DENSE,MISSION_GLIDE_SEGMENTS,WING_FOLDABLE,WING_HIGH_ASPECT,WING_MORPHING_MEMBRANE",2,5,12.919121454562084,67.55276772776418,5,2.3466843814418548,1.0,0.0,0.0,li_ion,"Conventional high-TRL Li-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,11.350984047985836,216.39926980618284,2456.3446595657647,0.0,0.0,aluminum_lithium,medium_stiff,0.02,carbon_composite,composite,0.7424147818313026,0.0,1.9633338369767501,1.207738117692021,0.7544235293879298,18.844210590223348,2.2386068785370634,3,80.47188918232627,5.2288979529571264,True,True,True,5.2288979529571264,"Bio-inspired by bat, albatross, this design is a heavy-lift VTOL rotorcraft concept. It uses 5 rotors, has an empty mass of 12.9 kg, and is configured to carry a payload of 67.6 kg (5.23:1 payload-to-aircraft mass ratio). The primary energy system is li-ion with a battery pack of 11.4 kg (~2456 Wh usable). The main load-bearing frame uses aluminum lithium (medium_stiff), with carbon_composite rotor blades and composite landing gear. Key bio-inspired features include an emphasis on energy-dense storage for long-range flight; mission planning that includes partial-power or glide segments to save energy; foldable wings that deploy after vertical takeoff for cruise efficiency; long, high-aspect-ratio lifting surfaces for efficient cruise; morphing membrane-like lifting surfaces that can change area and camber. In the synthetic DARPA Lift mission model, it cruises at about 18.8 m/s and climbs at roughly 2.2 m/s to around 350 ft. This design satisfies the basic DARPA Lift mass and payload constraints and is treated as a qualifying candidate with a nominal score of 5.23. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by bat, albatross, with 5 evenly spaced rotors and a compact central fuselage. Sleek aluminum lithium airframe, carbon composite rotor blades, and rugged composite landing gear. Subtle external cues of a li-ion energy system and integrated high-power modules, designed to carry a heavy payload under the belly. Aircraft shown in mid-flight at medium altitude, slightly angled to show top and side. high-resolution 3D-rendered digital image, realistic lighting, clear details, no motion blur, clean white or lightly blurred test-range background, no people, no logos, no text or numbers."