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@@ -61,3 +61,4 @@ missions_timeseries.csv filter=lfs diff=lfs merge=lfs -text
 Sample[[:space:]]dataset[[:space:]](n[[:space:]]=[[:space:]]10)/missions_timeseries.csv filter=lfs diff=lfs merge=lfs -text
 Sample[[:space:]]dataset[[:space:]](n[[:space:]]=[[:space:]]100)/missions_timeseries.csv filter=lfs diff=lfs merge=lfs -text
 Sample[[:space:]]dataset[[:space:]](n[[:space:]]=[[:space:]]1000)/missions_timeseries.csv filter=lfs diff=lfs merge=lfs -text
+Sample[[:space:]]dataset[[:space:]](n[[:space:]]=[[:space:]]10)[[:space:]]v1.0/missions_timeseries.csv filter=lfs diff=lfs merge=lfs -text

Sample dataset (n = 10) v1.0/designs.csv

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+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_cdcbb977a3,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_e58cb3539e,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_315c6623ba,"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_9b02e8a05b,"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_c671caf443,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_9379d01b6a,"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_6447703297,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_3005816f51,"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_cd2759c4dd,"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_12b9f22d9e,"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."

Sample dataset (n = 10) v1.0/missions.csv

@@ -0,0 +1,101 @@
+design_id,mission_id,wind_speed_kts,turbulence_index,success,failure_phase,failure_reason,rule_violation,total_time_s,time_takeoff_climb_s,time_loaded_cruise_s,time_empty_cruise_s,time_descent_landing_s,energy_used_Wh,battery_energy_remaining_Wh,payload_to_aircraft_ratio,is_qualifying_run,qualifying_score
+DLIFT_cdcbb977a3,MSN_8343960984,5.441782493412354,1.4358196083101717,True,,,,577.0,52.65560771945798,379.0,94.0,52.0,188.8303926538775,1077.1227547515603,2.6962117490934796,True,2.6962117490934796
+DLIFT_cdcbb977a3,MSN_e51a93f457,3.246104518305177,0.14507456525019602,True,,,,561.0,52.65560771945798,366.0,91.0,52.0,133.30093852639058,1132.6522088790687,2.6962117490934796,True,2.6962117490934796
+DLIFT_cdcbb977a3,MSN_853db4a2e9,21.130411097841186,1.2106924099115703,True,,,,729.0,52.65560771945798,500.0,125.0,52.0,193.4005257742892,1072.5526216311234,2.6962117490934796,True,2.6962117490934796
+DLIFT_cdcbb977a3,MSN_47b8c98cee,18.767983200914525,1.459673645969056,True,,,,700.0,52.65560771945798,477.0,119.0,52.0,201.62598437543187,1064.3271630300437,2.6962117490934796,True,2.6962117490934796
+DLIFT_cdcbb977a3,MSN_85ff257217,19.321422094562944,1.2441069963794922,True,,,,706.0,52.65560771945798,482.0,120.0,52.0,193.15357396477626,1072.799573440667,2.6962117490934796,True,2.6962117490934796
+DLIFT_cdcbb977a3,MSN_5cb3019d60,30.159741510877204,0.8660282178851431,True,,,,871.0,52.65560771945798,614.0,153.0,52.0,187.16892888027462,1078.7842185252314,2.6962117490934796,True,2.6962117490934796
+DLIFT_cdcbb977a3,MSN_5f2eed28b1,1.6038534279481775,0.3418474134773203,True,,,,550.0,52.65560771945798,357.0,89.0,52.0,139.98788373995419,1125.9652636655205,2.6962117490934796,True,2.6962117490934796
+DLIFT_cdcbb977a3,MSN_3c57bd2dc9,2.7927191923269623,0.34918632954154527,False,mission,energy_system_fault,energy_architecture_risk,156.0,52.65560771945798,104.0,0.0,0.0,104.61276707964294,1161.3403803258147,2.6962117490934796,False,0.0
+DLIFT_cdcbb977a3,MSN_df6370fc07,22.248955549254006,0.5472482684551263,True,,,,744.0,52.65560771945798,512.0,128.0,52.0,166.90177012423683,1099.05137728125,2.6962117490934796,True,2.6962117490934796
+DLIFT_cdcbb977a3,MSN_516c48afaf,7.332746077002069,0.40046673307367003,True,,,,591.0,52.65560771945798,390.0,97.0,52.0,147.53451640328547,1118.4186310021998,2.6962117490934796,True,2.6962117490934796
+DLIFT_e58cb3539e,MSN_26d36fe886,17.473094082229707,1.3270247308300538,True,,,,554.0,19.37709045682033,413.0,103.0,19.0,95.94165183030904,5359.608904333667,3.07035926882782,True,3.07035926882782
+DLIFT_e58cb3539e,MSN_43dab8942a,5.000505665472193,0.20944547928825946,True,,,,455.0,19.37709045682033,334.0,83.0,19.0,67.69911531913985,5387.851440844987,3.07035926882782,True,3.07035926882782
+DLIFT_e58cb3539e,MSN_5b8e6eef2a,18.864205138355164,1.1205207174783869,False,loaded_cruise,structural_overload,structural_margin_risk,268.0,19.37709045682033,249.0,0.0,0.0,67.08953998675564,5388.461016177209,3.07035926882782,False,0.0
+DLIFT_e58cb3539e,MSN_0f19377ada,12.669875529976384,1.4959886669837414,False,descent_landing,hard_touchdown,landing_profile_violation,503.0,19.37709045682033,379.0,94.0,11.0,95.06924081235488,5360.481315351565,3.07035926882782,False,0.0
+DLIFT_e58cb3539e,MSN_f0a5d9c39a,26.452375513680824,1.2916543644999987,False,descent_landing,hard_touchdown,landing_profile_violation,647.0,19.37709045682033,499.0,124.0,5.0,95.15120369767952,5360.399352466221,3.07035926882782,False,0.0
+DLIFT_e58cb3539e,MSN_4a776ad4f9,23.816842472371448,0.8946135460979607,False,mission,energy_system_fault,energy_architecture_risk,374.0,19.37709045682033,355.0,0.0,0.0,72.27995106443025,5383.270605099401,3.07035926882782,False,0.0
+DLIFT_e58cb3539e,MSN_9224a02e05,16.381746072463706,0.37712117997271977,True,,,,544.0,19.37709045682033,405.0,101.0,19.0,76.1170092329279,5379.433546931042,3.07035926882782,True,3.07035926882782
+DLIFT_e58cb3539e,MSN_8b00e0e030,32.98508014829334,1.0204251153847776,False,descent_landing,hard_touchdown,landing_profile_violation,771.0,19.37709045682033,587.0,146.0,19.0,96.53479962406922,5359.0157565399395,3.07035926882782,False,0.0
+DLIFT_e58cb3539e,MSN_bd53502ecd,26.28072298570634,1.152898098986169,False,descent_landing,hard_touchdown,landing_profile_violation,647.0,19.37709045682033,497.0,124.0,7.0,92.93264115316049,5362.617915010856,3.07035926882782,False,0.0
+DLIFT_e58cb3539e,MSN_3112c0930b,5.5355214020634405,0.004867974152593935,True,,,,459.0,19.37709045682033,337.0,84.0,19.0,63.78372729621422,5391.766828867737,3.07035926882782,True,3.07035926882782
+DLIFT_315c6623ba,MSN_5ad14ca0ad,17.00966621608148,0.10381877770257542,True,,,,1293.0,24.986955074115485,996.0,249.0,24.0,113.28962355518604,1089.3849728503221,3.2517110125515893,True,3.2517110125515893
+DLIFT_315c6623ba,MSN_a12007b866,26.804205025744572,0.1925871967496442,True,,,,1575.0,24.986955074115485,1222.0,305.0,24.0,123.04677273472338,1084.8992708424435,3.2517110125515893,True,3.2517110125515893
+DLIFT_315c6623ba,MSN_71356176bc,19.243125772323037,0.39758494341008865,True,,,,1348.0,24.986955074115485,1040.0,260.0,24.0,124.45680031207498,1084.247781289385,3.2517110125515893,True,3.2517110125515893
+DLIFT_315c6623ba,MSN_12b66df497,14.809827907031043,0.3176973081631231,True,,,,1244.0,24.986955074115485,957.0,239.0,24.0,118.76786067166698,1086.849821140883,3.2517110125515893,True,3.2517110125515893
+DLIFT_315c6623ba,MSN_67eef6b501,25.547587418149167,0.30172659508454386,True,,,,1533.0,24.986955074115485,1188.0,297.0,24.0,125.75969753888076,1083.6374545281649,3.2517110125515893,True,3.2517110125515893
+DLIFT_315c6623ba,MSN_da3be82ffc,34.83022748313131,0.9748170864591803,False,mission,time_limit_exceeded,time_limit,1801.0,24.986955074115485,1501.0,276.0,0.0,143.81976691685222,1080.9689895775466,3.2517110125515893,False,0.0
+DLIFT_315c6623ba,MSN_37d52c34fa,18.11515443624567,0.18150629380239858,False,mission,propulsion_architecture_fault,propulsion_architecture_risk,448.0,24.986955074115485,424.0,0.0,0.0,81.27680536039132,1123.187172029466,3.2517110125515893,False,0.0
+DLIFT_315c6623ba,MSN_99ab2fb3a5,20.590805146003166,0.3451720988948655,False,loaded_cruise,structural_overload,structural_margin_risk,101.0,24.986955074115485,77.0,0.0,0.0,70.18438622201732,1138.1048005593063,3.2517110125515893,False,0.0
+DLIFT_315c6623ba,MSN_39d2063576,22.088603504453463,0.34341267571673156,True,,,,1425.0,24.986955074115485,1102.0,275.0,24.0,124.68454088530255,1084.1401062153507,3.2517110125515893,True,3.2517110125515893
+DLIFT_315c6623ba,MSN_616efdf079,30.087239008881127,0.10628602483298016,False,mission,propulsion_architecture_fault,propulsion_architecture_risk,1141.0,24.986955074115485,1117.0,0.0,0.0,105.11188933100017,1102.5526155587131,3.2517110125515893,False,0.0
+DLIFT_9b02e8a05b,MSN_8bf638aeb7,6.4220812525531645,0.6939421026014511,True,,,,1097.0,38.64047489657557,817.0,204.0,38.0,162.83069286142216,718.5620870303721,3.63424721851783,True,3.63424721851783
+DLIFT_9b02e8a05b,MSN_dd72a48e4b,2.6384710931001276,1.2120333670975538,True,,,,1039.0,38.64047489657557,771.0,192.0,38.0,181.38746750209495,700.0053123896492,3.63424721851783,True,3.63424721851783
+DLIFT_9b02e8a05b,MSN_872d74ae46,3.4268054870560123,0.978217340997783,True,,,,1052.0,38.64047489657557,781.0,195.0,38.0,172.23373202112313,709.1590478706376,3.63424721851783,True,3.63424721851783
+DLIFT_9b02e8a05b,MSN_291d8e0e3f,0.5165249773477687,0.1398941642757539,True,,,,1011.0,38.64047489657557,748.0,187.0,38.0,133.93319133191181,747.4595885599022,3.63424721851783,True,3.63424721851783
+DLIFT_9b02e8a05b,MSN_0805d21f5d,8.27328216896123,0.609621086928708,True,,,,1128.0,38.64047489657557,842.0,210.0,38.0,160.95866104843168,720.4341188433363,3.63424721851783,True,3.63424721851783
+DLIFT_9b02e8a05b,MSN_84bba96a3d,30.26276379105754,1.353664298265823,False,loaded_cruise,structural_overload,structural_margin_risk,42.0,38.64047489657557,4.0,0.0,0.0,135.7664555069787,745.6263243847986,3.63424721851783,False,0.0
+DLIFT_9b02e8a05b,MSN_6d7de120d9,13.664761515573462,1.389777110339,True,,,,1228.0,38.64047489657557,922.0,230.0,38.0,198.9921180652805,682.4006618264752,3.63424721851783,True,3.63424721851783
+DLIFT_9b02e8a05b,MSN_d926ed2242,9.98372301314221,1.0448872554002437,True,,,,1158.0,38.64047489657557,866.0,216.0,38.0,181.0174756940317,700.3753041977731,3.63424721851783,True,3.63424721851783
+DLIFT_9b02e8a05b,MSN_9240a8e494,27.417653496950052,0.9928069679261178,True,,,,1602.0,38.64047489657557,1221.0,305.0,38.0,194.70832275188263,686.6844571398481,3.63424721851783,True,3.63424721851783
+DLIFT_9b02e8a05b,MSN_daad9d1cbc,6.6464253543673,0.3265513476212624,False,empty_cruise,control_saturation,,1011.0,38.64047489657557,820.0,153.0,0.0,137.43443385029465,743.9583460414809,3.63424721851783,False,0.0
+DLIFT_c671caf443,MSN_db8b44c4d0,9.126799346127148,1.004588962154744,False,mission,time_limit_exceeded,time_limit,1801.0,45.8260489013803,1470.0,286.0,0.0,137.250200322014,1741.036099454634,5.310863800196683,False,0.0
+DLIFT_c671caf443,MSN_787db6974f,9.296507938597383,0.19631742319118467,False,mission,time_limit_exceeded,time_limit,1801.0,45.8260489013803,1474.0,282.0,0.0,110.93899227807118,1767.347307498661,5.310863800196683,False,0.0
+DLIFT_c671caf443,MSN_7b7f1943c4,16.00286003996582,1.3935274975582712,False,mission,time_limit_exceeded,time_limit,1801.0,45.8260489013803,1657.0,99.0,0.0,153.86746227898982,1724.418837497662,5.310863800196683,False,0.0
+DLIFT_c671caf443,MSN_121313a1ec,0.32604099094862393,0.9317388832396392,True,,,,1695.0,45.8260489013803,1284.0,321.0,45.0,134.84155179853036,1743.4447479780868,5.310863800196683,True,5.310863800196683
+DLIFT_c671caf443,MSN_15fee06642,3.499343712360597,0.8064516061524409,True,,,,1771.0,45.8260489013803,1345.0,336.0,45.0,132.87206171675342,1745.4142380598225,5.310863800196683,True,5.310863800196683
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Sample dataset (n = 10) v1.0/missions_timeseries.csv

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