Matches in DBpedia 2014 for { ?s <http://dbpedia.org/property/moreGeneral> ?o. }
- 3I_Sky_Arrow moreGeneral "*Useful load: 250kg".
- AMX_International_AMX moreGeneral "Internal fuel capacity: 3,555l internal. * External fuel capacity: 2x 1,000l in inner wing and 2x 500l in outer wing.".
- ATR_72 moreGeneral "*Typical payload:".
- Aero_Spacelines_Super_Guppy moreGeneral "Cargo bay dimensions: 111 ft × 25 ft × 25 ft".
- Agusta_A129_Mangusta moreGeneral "Rotor systems: 4 blades on main rotor".
- Air_&_Space_18A moreGeneral "* Fuel capacity: 27.3 US gallons".
- Airbus_A330_MRTT moreGeneral "7200.0".
- Airbus_A400M_Atlas moreGeneral "*Max landing weight: 122,000 kg".
- American_Blimp_A-170 moreGeneral "*Lifting agent:' Helium *Gondola length: *Gondola width: *Gondola height: *Cabin length: *Cabin width: *Cabin height: *Lightsign length: *Lightsign height: *Lightsign Diagonal: *Lightsign Illumination:''' 369,600 LEDs + Internal illumination from two 1kW lights for night operation.".
- Antonov_An-225_Mriya moreGeneral "264.0".
- Antonov_An-71 moreGeneral "Powerplant: 1 x Rybinsk RD-38A turbojet, 31.9 kN".
- Atlas_Cheetah moreGeneral "Canard Area: 17.87 ft²".
- Avion_MAI_F-1 moreGeneral "*Take-off run: *Landing run:".
- Beechcraft_1900 moreGeneral "Fuel Capacity: 4,484 lb *Fuel type: Jet A recommended, others usable".
- Belite_Aircraft_Superlite moreGeneral "*Ballistic parachute: Second Chantz system".
- Bell_412 moreGeneral "Fuselage length: 43 ft".
- Bell_429_GlobalRanger moreGeneral "Cabin volume: 204 ft³".
- Bell_505_Jet_Ranger_X moreGeneral "*Useful load: 1500 lb".
- Bell_AH-1Z_Viper moreGeneral "Rotor systems: 4 blades on main rotor, 4 blades on tail rotor".
- Bell_AH-1_Cobra moreGeneral "Rotor system: 2 blades on main rotor, 2 blades on tail rotor * Fuselage length: 44 ft 5 in * Stub wing span: 10 ft 4 in".
- Bell_AH-1_Cobra moreGeneral "Rotor system: 2 blades on main rotor, 2 blades on tail rotor * Fuselage length: 44 ft 7 in * Stub wing span: 10 ft 4 in".
- Bell_AH-1_SuperCobra moreGeneral "Rotor systems: 2 blades on main rotor, 2 blades on tail rotor * Fuselage length: 45 ft 7 in * Stub wing span: 10 ft 9 in".
- Bell_AH-1_SuperCobra moreGeneral "Total engine output: 1,530 shp limited by helicopter drivetrain * Rotor systems: 2 blades on main rotor, 2 blades on tail rotor * Fuselage length: 45 ft 9 in * Stub wing span: 10 ft 9 in".
- Bell_HSL moreGeneral "*Rotor diameter' 51ft 6in *Rotor disc area 4,170sq ft".
- Bell_OH-58_Kiowa moreGeneral "Fuselage length: 34 ft 4.5 in".
- Bell_X-1 moreGeneral "Color : International Orange".
- Bell_XV-15 moreGeneral "Engine power ratings: ** 1,550 shp normal takeoff power ** 1,802 shp emergency power * Fuel weight: 1,436 lb".
- Beriev_A-40 moreGeneral "Takeoff boosters: 2x Kolesov RD36-35 turbojets, 23 kN each".
- Beriev_Be-10 moreGeneral "*Draught".
- Boeing-Sikorsky_RAH-66_Comanche moreGeneral "Fuselage length: 43.31 ft *Rotor systems: 5-bladed main rotor, 8-bladed fan-in-fin anti-torque system".
- Boeing_2707 moreGeneral "Max. landing weight:".
- Boeing_AH-64_Apache moreGeneral "Fuselage length: 49 ft 5 in *Rotor systems: 4 blade main rotor, 4 blade tail rotor in non-orthogonal alignment".
- Boeing_B-29_Superfortress moreGeneral "Zero-lift drag coefficient: 0.0241 * Drag area: 41.16 ft²".
- Boeing_B-47_Stratojet moreGeneral "Zero-lift drag coefficient: 0.0148 *Drag area: 21.13 ft² *Aspect ratio: 9.42".
- Boeing_B-52_Stratofortress moreGeneral "Fuel capacity: *Zero-lift drag coefficient: 0.0119 *Drag area: 47.60 *Aspect ratio: 8.56".
- Boeing_C-17_Globemaster_III moreGeneral "Fuel capacity: 35,546 U.S. gal".
- Boeing_EA-18G_Growler moreGeneral "Internal fuel capacity: 13,940 lb *External fuel capacity: : 9,774 lb".
- F_Super_Hornet moreGeneral "Internal fuel capacity: F/A-18E: 14,400 lb , F/A-18F: 13,550 lb * External fuel capacity: 5 × 480 gal tanks, totaling 16,380 lb".
- Boeing_KC-135_Stratotanker moreGeneral "Maximum Fuel Load: 200,000 lb".
- Boeing_KC-46_Pegasus moreGeneral "Fuel Capacity: 212,299 lb".
- Boeing_KC-46_Pegasus moreGeneral "Maximum Transfer Fuel Load: 207,672 lb".
- Boeing_KC-767 moreGeneral "Maximum Fuel Load: 160,660 lb".
- Boeing_RC-1 moreGeneral "*Cargo bay, four 26-foot diameter cylinders, 40+ feet long, designed to hold four standard cargo containers each".
- Boeing_Skyfox moreGeneral "** Internal fuel capacity: 3,191 litres ** Total fuel capacity: 4,932 litres".
- Boeing_Skyfox moreGeneral "Fuel capacity:".
- Boeing_VC-25 moreGeneral "Zero fuel weight: 526,500 lb".
- Boeing_X-37 moreGeneral "Power: Gallium arsenide solar cells with lithium-ion batteries *Payload bay:".
- Bombardier_Global_Express moreGeneral "Cabin length: 42.47 f * Cabin width : 8.17 ft * Cabin width : 6.92 ft * Cabin height: 6.25 ft * Cabin floor area: 317 ft² * Cabin Total Volume 1,884 ft³".
- Boulton_Paul_Bourges moreGeneral "Fuel capacity: 190 gallons".
- Breese-Wilde_Model_5 moreGeneral ", extra in containers were used on record flights.".
- Bristol_Brabazon moreGeneral "Fuel capacity 13,650 Imp gal".
- PAC_JF-17_Thunder moreGeneral "G-limit: +8 g / -3 g * Internal Fuel Capacity: 2,300 kg".
- COW_Biplane moreGeneral "Fuel capacity: 40 gallons plus 10 gallon gravity feed auxiliary".
- Canadair_CL-84 moreGeneral "*Maximum width over propeller tips:34 ft 8 in *Maximum height over propellers during wing tilt: 17 ft 1½ in".
- Caproni_Campini_N.1 moreGeneral "Piston engine drove a three-stage axial compressor for the thermojet with variable pitch vanes".
- Cessna_170 moreGeneral "Fuel capacity:".
- Cessna_421 moreGeneral "Pressurised 6-8 seat cabin twin.".
- Cierva_C.8 moreGeneral "Fuel capacity: 24 gallons .".
- Concorde moreGeneral "Maximum fuel load: * Maximum taxiing weight:".
- Consolidated_B-24_Liberator moreGeneral "Zero-lift drag coefficient: 0.0406 * Drag area: 42.54 ft² * Aspect ratio: 11.55".
- Consolidated_PBY_Catalina moreGeneral "Zero-lift drag coefficient: 0.0309 * Drag area: 43.26 ft² * Aspect ratio: 7.73".
- Convair_B-58_Hustler moreGeneral "Zero-lift drag coefficient: 0.0068 *Drag area: 10.49 ft² *Aspect ratio: 2.09".
- Convair_F-102_Delta_Dagger moreGeneral "Internal fuel capacity: 1,085 U.S. gal * External fuel capacity: 2 × 215 U.S. gal drop tanks".
- Convair_F-106_Delta_Dart moreGeneral "* Zero-lift drag coefficient: 0.0083 * Drag area: 5.8 ft² * Aspect ratio: 2.10".
- Curtiss_Thrush moreGeneral "*Oil capacity: 9 gallons".
- Custer_CCW-5 moreGeneral "*Maximum gross weight: 6,000 lb *Landing speed : 15 mph *'''Landing and take-off distances: 100 ft".
- Daimler_L20 moreGeneral "*Wing loading: 22.5 kg/m2".
- Dassault_Rafale moreGeneral "Fuel capacity: internal".
- Denel_Rooivalk moreGeneral "Internal fuel capacity: 1,854 L".
- Dornier_Do_212 moreGeneral ";Stabiliser Span: with 8° 30' dihedral".
- Douglas_C-133_Cargomaster moreGeneral "* Cargo deck : 86 ft 10 in".
- Douglas_XB-31 moreGeneral "Powerplant after later redesign: 4× Pratt & Whitney R-4360 "Wasp Major" radials, 3,000 hp each".
- Dyn'Aéro_CR.100 moreGeneral "*Maximum aerobatic weight: 760 kg".
- Northrop_Grumman_KC-45 moreGeneral "Maximum Fuel Capability: 245,000 lb *Cargo: 32 pallets".
- Eagle_Aircraft_Eagle_150 moreGeneral "292.8".
- Embraer_EMB_120_Brasilia moreGeneral "Maximum Landing Weight: 11,250 kg".
- Embraer_EMB_312_Tucano moreGeneral "Internal fuel:".
- Embraer_KC-390 moreGeneral "Fuel capacity: 37.4 tons".
- Emelyanov_KIM-3_Stakanovets moreGeneral "*Wing loading: 19.7 kg/m²".
- English_Electric_Ayr moreGeneral "All weights estimated".
- Eta_(glider) moreGeneral "*Maximum wing loading: 44.8 kg/m2".
- Eurocopter_Tiger moreGeneral "Internal fuel capacity: 1,080 kg".
- Eurofighter_Typhoon moreGeneral "Fuel capacity: internal".
- Extra_EA-300 moreGeneral "Fuel capacity: 52.7 U.S. gal".
- FFA_AS-202_Bravo moreGeneral "Landing gear: fixed tricycle".
- FFA_AS-202_Bravo moreGeneral "Max landing weight : AS 202-18A4 1,050 kg".
- Fairchild_Republic_A-10_Thunderbolt_II moreGeneral "Internal fuel capacity: 11,000 lb".
- Fairchild_T-46 moreGeneral "Internal fuel capacity: 200 US Gal".
- Fairey_Long-range_Monoplane moreGeneral "Mean chord: 11 ft".
- Fajr_F.3 moreGeneral "75.0".
- Fokker_Dr.I moreGeneral "Zero-lift drag coefficient: 0.0323 *Drag area: 0.62 m² *Aspect ratio: 4.04".
- Fouga_CM.10 moreGeneral "*Cargo hold capacity:".
- Gee_Bee_Model_R moreGeneral "Aspect ratio: 6.1 , *Incidence: 2.5 Degrees".
- Grumman_EF-111A_Raven moreGeneral "Zero-lift drag coefficient: 0.0186 *Drag area: 9.36 ft² *Aspect ratio: 7.56 unswept; 1.95 fully swept".
- General_Dynamics_F-111C moreGeneral "Zero-lift drag coefficient: 0.0186 * Drag area: 9.36 ft² * Aspect ratio: spread: 7.56, swept: 1.95".
- General_Dynamics_F-111_Aardvark moreGeneral "Zero-lift drag coefficient: 0.0186 * Drag area: 9.36 ft² * Aspect ratio: spread: 7.56, swept: 1.95".
- 39 moreGeneral "Fuel capacity: 81 gallons".
- Grob_G_115 moreGeneral "Max Fuel Capacity: 143 l".
- Grumman_A-6_Intruder moreGeneral "Zero-lift drag coefficient: 0.0144".
- Grumman_F-14_Tomcat moreGeneral "Maximum fuel capacity: 16,200 lb internal; 20,000 lb with 2x 267 gallon external tanks".