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,battery_nominal_voltage_V,battery_max_power_W,supercap_mass_kg,supercap_energy_Wh,supercap_max_power_W,motor_type,motor_efficiency,esc_efficiency,esc_current_rating_A,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,wing_foldable,wing_deploy_time_s,wing_deploy_failure_risk,image_prompt,design_success_rate,design_qualifying_rate,design_rule_penalty_rate,design_rank_score,design_stars
DLIFT_186142ea7d,harpy_eagle,"LIFT_BURST_POWER,LIFT_HIGH_CONTINUOUS,PAYLOAD_CENTRAL_TALON",1,3,21.26938124699791,57.34675561410429,6,2.1310596998296174,2.3533989748458226,18.16705265098237,0.0,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,6.797296377167434,182.38377755504564,1239.716590429023,39.74193418585944,9357.625783792062,0.07960790905159087,3.184316362063635,127.3726544825454,electric_brushless_outunner,0.8101439266950624,0.9743572358052935,50.17234716474934,carbon_composite,light_stiff,0.01,glass_composite,steel,0.49973927897133646,0.0,1.383898525813863,2.9997059385351537,0.512997519356122,21.11638503665616,4.792557579952907,4,78.6161368611022,2.6962117490934796,True,True,True,2.6962117490934796,"Bio-inspired by harpy_eagle, this design is a heavy-lift VTOL rotorcraft concept. It uses 6 rotors, has an empty mass of 21.3 kg, and carries a payload of 57.3 kg (2.70:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 6.8 kg battery (~1240 Wh usable) at about 40 V. Estimated battery peak power is ~9.4 kW. It also includes ~0.1 kg of supercapacitors (~3 Wh) that can provide high peak power (up to ~0.1 kW). The primary propulsion architecture is pure rotor electric, using electric brushless outunner motors with a nominal electronic speed controller rating of ~50 A. The main 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; a central payload cradle aligned with the center of gravity. In the synthetic mission model, it cruises at about 21.1 m/s and climbs at about 4.8 m/s to around 350 ft. This design satisfies the basic 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,False,0.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by harpy_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.",0.0,0.0,1.0,0.0,3
DLIFT_a2afffcfd2,golden_eagle,"LIFT_BURST_POWER,LIFT_HIGH_CONTINUOUS,PAYLOAD_CENTRAL_TALON",1,3,18.72043005127034,65.17654082146296,6,2.4065631291911926,2.761728347372879,17.947594122237227,0.0,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,4.419721491215087,246.69959637118455,1090.343507955812,74.65487460629072,9273.480451249286,2.961699190894513,118.46796763578052,4738.718705431221,electric_brushless_outunner,0.8194458780041052,0.9494783344663124,43.97422856303852,titanium_alloy,heavy_robust,0.005,carbon_composite,composite,0.5859998955209822,0.0,1.495083072449116,4.543506016493836,0.7685822287867354,7.308573408382044,2.4281439108376706,6,83.8969708727333,3.4815728400983064,True,True,True,3.4815728400983064,"Bio-inspired by golden_eagle, this design is a heavy-lift VTOL rotorcraft concept. It uses 6 rotors, has an empty mass of 18.7 kg, and carries a payload of 65.2 kg (3.48:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 4.4 kg battery (~1090 Wh usable) at about 75 V. Estimated battery peak power is ~9.3 kW. It also includes ~3.0 kg of supercapacitors (~118 Wh) that can provide high peak power (up to ~4.7 kW). The primary propulsion architecture is pure rotor electric, using electric brushless outunner motors with a nominal electronic speed controller rating of ~44 A. The main 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 payload cradle aligned with the center of gravity. In the synthetic mission model, it cruises at about 7.3 m/s and climbs at about 2.4 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.48. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,False,0.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by golden_eagle, with 6 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.",0.0,0.0,1.0,0.0,3
DLIFT_1db7e6427c,"bat,bee,golden_eagle","LIFT_BURST_POWER,LIFT_HIGH_CONTINUOUS,LIFT_UNSTEADY_AERO,PAYLOAD_CENTRAL_TALON,STAB_DISTRIBUTED_THRUST,WING_FOLDABLE,WING_MORPHING_MEMBRANE",3,7,17.683741562706025,60.12501644221612,20,1.4895592618943285,2.9024082397211233,10.166602054898558,0.2087277287280303,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,9.741218349745656,184.16684865946044,1794.0094855763673,92.53821785149832,9002.338686328441,0.20585511135830825,8.23420445433233,329.3681781732932,electric_brushless_outunner,0.8158741175187062,0.9566002828445324,7.883475808776741,steel_truss,heavy_robust,0.01,carbon_composite,titanium,0.4967532282436646,0.0,1.7588432694268972,3.477077237467018,0.9770898837778117,14.471221218922562,2.4575577844372263,3,77.80875800492214,3.4000166892857253,True,True,True,3.4000166892857253,"Bio-inspired by bat, bee, golden_eagle, this design is a heavy-lift VTOL rotorcraft concept. It uses 20 rotors, has an empty mass of 17.7 kg, and carries a payload of 60.1 kg (3.40:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 9.7 kg battery (~1794 Wh usable) at about 93 V. Estimated battery peak power is ~9.0 kW. It also includes ~0.2 kg of supercapacitors (~8 Wh) that can provide high peak power (up to ~0.3 kW). The primary propulsion architecture is pure rotor electric, using electric brushless outunner motors with a nominal electronic speed controller rating of ~8 A. The main 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; unsteady aerodynamics for better hover and low-speed lift; a central payload cradle aligned with the center of gravity; many smaller rotors for fine-grained control and redundancy; foldable wings that deploy after vertical takeoff for cruise efficiency. It uses foldable wings that deploy after takeoff. The wing deployment time is ~7.8 s with a synthetic deployment failure risk of ~12.0%. In the synthetic mission model, it cruises at about 14.5 m/s and climbs at about 2.5 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.40. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,True,7.782408464607252,0.12,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by bat, bee, golden_eagle, 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.",0.0,0.0,1.0,0.0,3
DLIFT_11dd30de89,"tiger,osprey,cheetah","LIFT_BURST_POWER,MISSION_MULTI_GAIT,PAYLOAD_DAMPED,PAYLOAD_SLING_LOAD,STAB_COMPLIANT_SPINE,STAB_GUST_REJECTION,STRUCT_ROBUST_GEAR,STRUCT_TENDON_CABLES",3,8,17.476451188404727,70.94750087366516,5,1.1404172194183286,2.260044554008121,16.588333465666,0.0,li_s,Experimental lithium-sulfur chemistry with very high energy density but lower maturity and stability.,very_high,medium,low,0.05,5.796751245540015,302.0511696699091,1750.915494000864,53.37532948487298,7034.906621906158,2.5242170448511065,100.96868179404426,4038.74727176177,electric_multirotor_plus_pusher,0.9090615409904187,0.9628708401216802,46.34843678492456,carbon_composite,light_stiff,0.01,aluminum,steel,0.44855776580981266,0.652857141953873,1.2,3.206455961119727,1.996471028806059,14.649991539157126,3.888879127613631,5,88.42395206206989,4.059605700769353,True,True,True,4.059605700769353,"Bio-inspired by tiger, osprey, cheetah, this design is a heavy-lift VTOL rotorcraft concept. It uses 5 rotors, has an empty mass of 17.5 kg, and carries a payload of 70.9 kg (4.06:1 payload-to-aircraft mass ratio). The energy system is li-s with a 5.8 kg battery (~1751 Wh usable) at about 53 V. Estimated battery peak power is ~7.0 kW. It also includes ~2.5 kg of supercapacitors (~101 Wh) that can provide high peak power (up to ~4.0 kW). The primary propulsion architecture is rotor plus pusher, using electric multirotor plus pusher motors with a nominal electronic speed controller rating of ~46 A. The main 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; multiple flight modes to optimize heavy-load and unloaded segments; 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; enhanced gust rejection and stability control for windy conditions. In the synthetic mission model, it cruises at about 14.6 m/s and climbs at about 3.9 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 4.06. ",rotor_plus_pusher,multirotor,pusher_propeller,0.35343440529885994,1.05,0.9,0.01,False,0.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by tiger, osprey, cheetah, with 5 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-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.",0.0,0.0,1.0,0.0,3
DLIFT_79104556e5,"albatross,osprey,bat","LIFT_ENERGY_DENSE,MISSION_GLIDE_SEGMENTS,PAYLOAD_DAMPED,PAYLOAD_SLING_LOAD,STAB_GUST_REJECTION,WING_FOLDABLE,WING_HIGH_ASPECT,WING_MORPHING_MEMBRANE",3,8,19.05722469884954,52.05830458473068,12,1.390020318485322,1.0,0.0,0.0,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,10.827258840925902,233.14238213728922,2524.2929181904897,34.623900955783945,28031.71579727542,0.0,0.0,0.0,electric_multirotor_plus_pusher,0.8171514511654963,0.945704134467075,77.78233560277471,carbon_composite,light_stiff,0.01,aluminum,titanium,0.4300939412114464,0.0,1.2,0.9996659308393895,1.8221152851946336,5.515602995723967,2.0594413089228354,3,71.11552928358022,2.731683411796754,True,True,True,2.731683411796754,"Bio-inspired by albatross, osprey, bat, this design is a heavy-lift VTOL rotorcraft concept. It uses 12 rotors, has an empty mass of 19.1 kg, and carries a payload of 52.1 kg (2.73:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 10.8 kg battery (~2524 Wh usable) at about 35 V. Estimated battery peak power is ~28.0 kW. The primary propulsion architecture is rotor plus pusher, using electric multirotor plus pusher motors with a nominal electronic speed controller rating of ~78 A. The main frame uses carbon composite (light_stiff), with aluminum 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; 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. It uses foldable wings that deploy after takeoff. The wing deployment time is ~2.7 s with a synthetic deployment failure risk of ~9.3%. In the synthetic mission model, it cruises at about 5.5 m/s and climbs at about 2.1 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 2.73. ",rotor_plus_pusher,multirotor,pusher_propeller,0.20631243340446412,1.05,0.9,0.01,True,2.68189584071928,0.09278882320895054,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by albatross, osprey, bat, with 12 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.",0.0,0.0,0.9,0.019999999999999997,3
DLIFT_ae222fd3a2,dragonfly,"STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION",1,2,13.383179037696928,71.7073044688947,20,1.5164945575170312,1.0,0.0,0.0,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,7.236530173175778,226.27576535729497,1637.4514034665074,32.59416168221386,12317.335064326397,0.0,0.0,0.0,electric_multirotor_plus_micro_turbojet,0.8708887490633388,0.9558796655985721,28.068754366815885,carbon_composite,light_stiff,0.01,carbon_composite,composite,0.4195147197243459,0.0,1.2,2.905032116884856,0.5038602435080877,8.536891634453221,2.796294334174036,6,85.09048350659164,5.358017274289906,True,True,True,5.358017274289906,"Bio-inspired by dragonfly, this design is a heavy-lift VTOL rotorcraft concept. It uses 20 rotors, has an empty mass of 13.4 kg, and carries a payload of 71.7 kg (5.36:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 7.2 kg battery (~1637 Wh usable) at about 33 V. Estimated battery peak power is ~12.3 kW. The primary propulsion architecture is rotor plus small jet, using electric multirotor plus micro turbojet motors with a nominal electronic speed controller rating of ~28 A. The main frame uses carbon composite (light_stiff), with carbon composite rotor blades and composite 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 mission model, it cruises at about 8.5 m/s and climbs at about 2.8 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 5.36. ",rotor_plus_small_jet,multirotor,small_jet,0.13307976530145282,1.15,0.85,0.03,False,0.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by dragonfly, with 20 evenly spaced rotors and a compact central fuselage. Sleek carbon composite airframe, 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.",0.6,0.6,0.4,0.6,5
DLIFT_3d85481be6,"osprey,cheetah,harpy_eagle","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",3,9,19.128037457262288,72.19392072628818,10,2.0317271900241836,2.5993411226066057,11.643474681708465,0.0,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,4.414499280374203,246.28742843642104,1087.2356755977937,82.70956164030078,11066.706290882521,2.6089990382485766,104.35996152994306,4174.398461197723,electric_multirotor_plus_pusher,0.7925877171122497,0.9491677628937116,25.36702542995526,carbon_composite,light_stiff,0.01,glass_composite,titanium,0.6108284054085863,0.2674684590948292,1.2,3.23114552708662,2.4552410423802398,10.445949410178986,4.451289094829386,4,91.32195818355046,3.77424609751998,True,True,True,3.77424609751998,"Bio-inspired by osprey, cheetah, harpy_eagle, this design is a heavy-lift VTOL rotorcraft concept. It uses 10 rotors, has an empty mass of 19.1 kg, and carries a payload of 72.2 kg (3.77:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 4.4 kg battery (~1087 Wh usable) at about 83 V. Estimated battery peak power is ~11.1 kW. It also includes ~2.6 kg of supercapacitors (~104 Wh) that can provide high peak power (up to ~4.2 kW). The primary propulsion architecture is rotor plus pusher, using electric multirotor plus pusher motors with a nominal electronic speed controller rating of ~25 A. The main 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; strong continuous lifting capacity for heavy payloads; multiple flight modes to optimize heavy-load and unloaded segments; a central 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 mission model, it cruises at about 10.4 m/s and climbs at about 4.5 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.77. ",rotor_plus_pusher,multirotor,pusher_propeller,0.20698534075329356,1.05,0.9,0.01,False,0.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by osprey, cheetah, harpy_eagle, with 10 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.",0.0,0.0,1.0,0.0,3
DLIFT_8216f68b93,"albatross,osprey,cheetah","LIFT_BURST_POWER,LIFT_ENERGY_DENSE,MISSION_GLIDE_SEGMENTS,MISSION_MULTI_GAIT,PAYLOAD_DAMPED,PAYLOAD_SLING_LOAD,STAB_COMPLIANT_SPINE,STAB_GUST_REJECTION,STRUCT_TENDON_CABLES,WING_HIGH_ASPECT",3,10,15.910899305941191,66.42393968335877,8,1.115110089158623,2.213972451807986,9.763298891263954,0.0,li_s,Experimental lithium-sulfur chemistry with very high energy density but lower maturity and stability.,very_high,medium,low,0.05,10.321585570293031,391.1053593970647,4036.8274340170133,43.686875322112094,15600.82436000075,1.4999931782205898,59.999727128823594,2399.9890851529435,electric_brushless_outunner,0.8956045176466855,0.9703911726061754,88.36705055848,steel_truss,heavy_robust,0.01,glass_composite,steel,0.3301771644018054,0.34114915079174846,1.4998424340249419,3.809062852100728,1.9568542146650123,7.089559946100321,3.083684268347892,4,82.33483898929995,4.174744519849724,True,True,True,4.174744519849724,"Bio-inspired by albatross, osprey, cheetah, this design is a heavy-lift VTOL rotorcraft concept. It uses 8 rotors, has an empty mass of 15.9 kg, and carries a payload of 66.4 kg (4.17:1 payload-to-aircraft mass ratio). The energy system is li-s with a 10.3 kg battery (~4037 Wh usable) at about 44 V. Estimated battery peak power is ~15.6 kW. It also includes ~1.5 kg of supercapacitors (~60 Wh) that can provide high peak power (up to ~2.4 kW). The primary propulsion architecture is pure rotor electric, using electric brushless outunner motors with a nominal electronic speed controller rating of ~88 A. The main 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 to optimize heavy-load and unloaded segments; damped payload mounting to reduce oscillations during flight; a sling-load style payload mount hanging beneath the airframe. In the synthetic mission model, it cruises at about 7.1 m/s and climbs at about 3.1 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 4.17. ",pure_rotor_electric,multirotor,none,0.0,1.0,1.0,0.0,False,0.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by albatross, osprey, cheetah, with 8 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-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.",0.1,0.1,0.9,0.1,4
DLIFT_88212b4dde,"albatross,dragonfly,bat","LIFT_ENERGY_DENSE,MISSION_GLIDE_SEGMENTS,STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION,WING_FOLDABLE,WING_HIGH_ASPECT,WING_MORPHING_MEMBRANE",3,7,20.157045569162197,66.76734183211451,15,2.2810669291659202,1.0,0.0,0.0,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,6.355559282857166,244.29029040914637,1552.601422921723,95.1971835361851,9081.732915430897,0.0,0.0,0.0,electric_multirotor_plus_pusher,0.9003445977759189,0.9572228886366955,8.46103655578082,carbon_composite,light_stiff,0.01,glass_composite,titanium,0.8742508561954588,0.0,1.2,3.242018326780159,0.9710539702317507,20.662003740529023,2.7004834720051805,2,86.9243874012767,3.312357537865586,True,True,True,3.312357537865586,"Bio-inspired by albatross, dragonfly, bat, this design is a heavy-lift VTOL rotorcraft concept. It uses 15 rotors, has an empty mass of 20.2 kg, and carries a payload of 66.8 kg (3.31:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 6.4 kg battery (~1553 Wh usable) at about 95 V. Estimated battery peak power is ~9.1 kW. The primary propulsion architecture is rotor plus pusher, using electric multirotor plus pusher motors with a nominal electronic speed controller rating of ~8 A. The main frame uses carbon composite (light_stiff), with glass 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; 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; long, high-aspect-ratio lifting surfaces for efficient cruise. It uses foldable wings that deploy after takeoff. The wing deployment time is ~2.9 s with a synthetic deployment failure risk of ~12.0%. In the synthetic mission model, it cruises at about 20.7 m/s and climbs at about 2.7 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.31. ",rotor_plus_pusher,multirotor,pusher_propeller,0.22369911445687723,1.05,0.9,0.01,True,2.9279488564381584,0.12,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by albatross, dragonfly, 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-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.",0.5,0.5,0.5,0.5,4
DLIFT_057a49a2d7,"bee,dragonfly","LIFT_UNSTEADY_AERO,STAB_DISTRIBUTED_THRUST,STAB_GUST_REJECTION",2,3,14.275730283320435,56.88266357992639,23,1.927836730905342,1.0,0.0,0.09958999458608006,li_ion,"Conventional high-TRL lithium-ion pack for VTOL drones, good power and proven reliability.",medium_high,high,high,0.01,11.796867543966723,237.9667543189523,2807.2622805683513,56.93455475063206,23855.104229438195,0.0,0.0,0.0,electric_multirotor_plus_pusher,0.8067754612404923,0.9797286089853857,14.197217373503412,aluminum_lithium,medium_stiff,0.02,carbon_composite,titanium,0.3460683865418145,0.0,1.2,0.5965981359837482,1.135375140731193,14.31458401905105,4.854411738713141,3,71.15839386324683,3.9845711883746713,True,True,True,3.9845711883746713,"Bio-inspired by bee, dragonfly, this design is a heavy-lift VTOL rotorcraft concept. It uses 23 rotors, has an empty mass of 14.3 kg, and carries a payload of 56.9 kg (3.98:1 payload-to-aircraft mass ratio). The energy system is li-ion with a 11.8 kg battery (~2807 Wh usable) at about 57 V. Estimated battery peak power is ~23.9 kW. The primary propulsion architecture is rotor plus pusher, using electric multirotor plus pusher motors with a nominal electronic speed controller rating of ~14 A. The main frame uses aluminum lithium (medium_stiff), with carbon composite rotor blades and titanium landing gear. Key bio-inspired features include unsteady aerodynamics for better hover and low-speed lift; many smaller rotors for fine-grained control and redundancy; enhanced gust rejection and stability control for windy conditions. In the synthetic mission model, it cruises at about 14.3 m/s and climbs at about 4.9 m/s to around 350 ft. This design satisfies the basic mass and payload constraints and is treated as a qualifying candidate with a nominal score of 3.98. ",rotor_plus_pusher,multirotor,pusher_propeller,0.3685419621733098,1.05,0.9,0.01,False,0.0,0.0,"Futuristic heavy-lift VTOL rotorcraft drone bio-inspired by bee, dragonfly, with 23 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.",0.8,0.8,0.0,0.8400000000000001,5