Matches in DBpedia 2014 for { ?s <http://dbpedia.org/property/moreGeneral> ?o. }
- Piper_PA-44_Seminole moreGeneral "Maximum Ramp Weight: 3 816 lb".
- Piper_PA-47_PiperJet moreGeneral "*Full fuel payload: intended to be 800 lbs +/-5%".
- Pipistrel_Sinus moreGeneral "* Fuel capacity: 2×30 L * Baggage capacity:".
- Polikarpov_TIS moreGeneral "*Fuel capacity:".
- Reaction_Engines_A2 moreGeneral "Fuel capacity: 198 tonnes liquid hydrogen".
- Republic_F-105_Thunderchief moreGeneral "Zero-lift drag coefficient: 0.0173 *Drag area: 6.65 ft² *Aspect ratio: 3.16".
- Robinson_R22 moreGeneral "Main tank total capacity: 19.8 US gallons * Main tank usable capacity: 19.2 US gallons * Optional aux tank total capacity: 10.9 US gallons * Optional aux tank usable capacity: 10.5 US gallons".
- Robinson_R44 moreGeneral "Fuel: 100 low lead fuel or 100/130. *Main tank capacity: 31.6 US gallons *Main tank usable fuel: 30.6 US gallons *Auxiliary tank capacity: 18.5 US gallons *Auxiliary tank usable fuel: 18.3 US gallons".
- Rockwell_B-1_Lancer moreGeneral "Fuel capacity, optional: 10,000 U.S. gal fuel tank for 1–3 internal weapons bays each".
- SOCATA_TBM moreGeneral "Max payload full fuel: 385 kg".
- Saab_JAS_39_Gripen moreGeneral "144.0".
- Scaled_Composites_Model_367_BiPod moreGeneral "1.2".
- Schleicher_ASW_24 moreGeneral "* Cockpit width: * Cockpit height:".
- Schleicher_K_10 moreGeneral "*Wing loading: 25.5 kg/m2".
- Schleicher_Ka_3 moreGeneral "*Wing loading: 19.5 kg/m2 maximum".
- Schneider_ES-49 moreGeneral "*'''Wing loading".
- Schneider_ES-54_Gnome moreGeneral "*Wing loading: 20.2 kg/m2".
- Schneider_ES-56_Nymph moreGeneral "*Wing loading: 23.8 kg/m2".
- Schneider_ES-57_Kingfisher moreGeneral "*Wing loading: 20.7 kg/m2".
- Schneider_ESG_31_Schlesierland moreGeneral "*Wing loading: 13.5 kg/m²".
- Schneider_Grunau_8 moreGeneral "* Wing loading: 16.35 kg/m²".
- Schneider_Moazagotl moreGeneral "*Wing loading: 13.5 kg/m² without ballast, 16.0 kg/m² ballasted".
- Schweizer_X-26_Frigate moreGeneral "Propeller: Ole Fahlin four-blade, 8 inch chord, fixed-pitch 100 inch diameter *Wing aspect ratio: 18 *Fuel Capacity: 20 gallons".
- Schweizer_X-26_Frigate moreGeneral "Wing aspect ratio: 18".
- Shenyang_J-15 moreGeneral "444.0".
- Shenyang_J-6 moreGeneral "Fuel capacity: 1,800 kg".
- ShinMaywa_US-2 moreGeneral "Boundary layer enhancement provided by 1,015 kW LHTEC T800".
- Shin_Meiwa_US-1A moreGeneral "plus 1× General Electric T58 gas turbine, 1,104 kW driving boundary layer control system".
- Short_Mayo_Composite moreGeneral "* Normal composite launch weight: 20,800 lb * Record composite launch weight: 26,800 lb".
- Short_Mayo_Composite moreGeneral "*Takeoff weight : 27,700 lb".
- Short_SB.1 moreGeneral "* Leading-edge sweep: 42.25°".
- Short_SB.5 moreGeneral "Fuel capacity: 300 Imp. gallons".
- Short_SC.1 moreGeneral "* Powerplant: ** Lift: 4× Rolls-Royce RB108 turbojets, 2,130 lbf each ** Forward flight: 1× Rolls-Royce RB108 turbojet, 2,130 lbf".
- Short_Sperrin moreGeneral "Fuel capacity: 6,200 gallons".
- Sikorsky_CH-148_Cyclone moreGeneral "Fuselage length: 56 ft 2 in * Fuselage width: 17 ft 3 in".
- Sikorsky_CH-53E_Super_Stallion moreGeneral "Rotor systems: 7 blades on main rotor, 4 blades on anti-torque tail rotor".
- Sikorsky_CH-53K_Super_Stallion moreGeneral "Rotor systems: 7 blades on main rotor, 4 blades on tail rotor".
- Sikorsky_CH-53_Sea_Stallion moreGeneral "Width : 28 ft 4 in *Width : 15 ft 6 in *Rotor systems: 6 blades on main rotor".
- Sikorsky_Ilya_Muromets moreGeneral "* Fuel and oil: 600 kg".
- Sikorsky_MH-53 moreGeneral "Rotor system: 6 blades".
- Sikorsky_S-10 moreGeneral "Wing Load: 22kg/m²".
- Sikorsky_S-10 moreGeneral "Wing Load: 24.3kg/m²".
- Sikorsky_S-61R moreGeneral "Rotor system: 5 blades".
- Sikorsky_S-67_Blackhawk moreGeneral "Rotor system: 5 blades on main rotor, 5 blades on tail rotor * Fuselage length: * Fuselage height: * Stub wing span:".
- Sikorsky_S-69 moreGeneral "345".
- Sikorsky_S-69 moreGeneral "Rotor: 2 three-bladed co-axial, with 30 inch separation".
- Sikorsky_S-70 moreGeneral "Fuel, internal: 1,360 L * Auxiliary Fuel: 2x 700 L tanks internally, 1,705 L tank on each inboard pylon and 872 L tank on each outboard pylon, or 1,705 L tank on each pylon".
- Sikorsky_S-72 moreGeneral "* Take-off weight without auxiliary jets: 8,300 kg * Empty weight without auxiliary jets: 6,535 kg".
- Sikorsky_S-92 moreGeneral "Fuselage length: 56 ft 2 in *Fuselage width: 17 ft 3 in *Rotor systems: Main rotor has 4 blades. From the main gearbox a set of driveshafts connect to the tail gearbox to turn the 4-blade tail rotor. *Cabin dimensions: 20 ft long by 6.6 ft tall".
- Sikorsky_X2 moreGeneral "Rotor configuration: 2 four-bladed co-axial".
- Softeks_V-24_Lastochka moreGeneral "12000.0".
- Soko_G-2_Galeb moreGeneral "* Internal fuel load: 780 kg * External fuel load: Up to 340 kg in two wing-tip drop tanks".
- Solar_Impulse moreGeneral "Take-off speed:".
- Sopwith_Camel moreGeneral "Zero-lift drag coefficient: 0.0378 *Drag area: *Aspect ratio: 4.11".
- Sopwith_Salamander moreGeneral "Fuel: 29 Imperial gallons".
- SpaceShipOne moreGeneral "87.0".
- Spectrum_S-33_Independence moreGeneral "Interior Height: 5 ft 0 in * Interior Width: 5 ft 0 in * Interior Length : 18 ft".
- Spectrum_S-40_Freedom moreGeneral "* Interior Height: 6 ft 0 in * Interior Width: 6 ft 0 in * Interior Length : 16 ft 0 in * Interior Length : 21 ft 2 in".
- Spijker_V.2 moreGeneral "*Oil capacity: 25 L".
- Spijker_V.3 moreGeneral "*Oil capacity: 18 L".
- Starr_Bumble_Bee_II moreGeneral "Fuel capacity: 3 US gallons".
- Stemme_S6 moreGeneral "*Wing loading: 48.79 kg/m2".
- HAL_FGFA moreGeneral "Fuel capability: 10,300 kg".
- Sukhoi_PAK_FA moreGeneral "Fuel capacity: 10,300 kg".
- Sukhoi_Su-17 moreGeneral "Fuel capacity: 3,770 kg".
- Sukhoi_Su-24 moreGeneral "Fuel capacity: 11,100 kg".
- Sukhoi_Su-27 moreGeneral "Fuel capacity: 9,400 kg internally".
- Sukhoi_Su-27 moreGeneral "Leading edge sweep: 42°".
- Sukhoi_Su-28 moreGeneral "* Fuel capacity : 2,750 kg * Fuel capacity : 4 × 1,150 kg drop tanks".
- Sukhoi_Su-33 moreGeneral "444.0".
- Sukhoi_Su-34 moreGeneral "Internal fuel: 12,100 kg".
- Sukhoi_Su-35 moreGeneral "Fuel capacity:".
- Sukhoi_Su-47 moreGeneral "Thrust vectoring: ±20° at 30° per second in pitch and yaw".
- Sukhoi_Su-7 moreGeneral "*Fuel capacity: 3,220 kg".
- Supermarine_Seagull_(1948) moreGeneral "Span with wings folded: 23 ft 6 in".
- AgustaWestland_T129 moreGeneral "Rotor systems: 5 blades on main rotor".
- Tarrant_Tabor moreGeneral "Fuel capacity: 10,000 lb".
- Technoavia_Rysachok moreGeneral "*Maximum payload:1,570 kg".
- Terrafugia_Transition moreGeneral "Cockpit width: at the shoulder * Fuel capacity: , * Length on road: with elevator up * Width on road: with wings folded * Height on road: * Rear wheel drive on road".
- The_Airplane_Factory_Sling moreGeneral "Fuel Capacity: 39.6 U.S. gallons *Baggage Capacity: 77 lb".
- Thorp_T-211 moreGeneral "* Fuel capacity: 21 gal usable * Baggage capacity: 40 lb".
- Travel_Air_5000 moreGeneral "425".
- Tupolev_Tu-134 moreGeneral "Fuselage diameter: *Fuel capacity:".
- Tupolev_Tu-244 moreGeneral "480.0".
- Tupolev_Tu-28 moreGeneral "Maximum g-loading: 2.5 g * Maximum fuel load: est. 13,600 kg".
- Van_Berkel_W-B moreGeneral "*Useful load: 950 kg , of which approximately 610 kg is fuel.".
- Vought_F-8_Crusader moreGeneral "Zero-lift drag coefficient: 0.0133 *Drag area: 5.0 ft² *Fuel capacity:".
- Vought_XF8U-3_Crusader_III moreGeneral "Fuel capacity: 2,000 US gal".
- Waco_CG-4 moreGeneral "Max take off : 9,000 lb".
- Westland_Wizard moreGeneral "*Oil capacity: 5 gallons".
- Westland_Wizard moreGeneral "Fuel capacity: 68 gallons".
- Yakovlev_Yak-18T moreGeneral "weight limit 1,510 kg for aerobatics".
- Yakovlev_Yak-30_(1960) moreGeneral "Basic fuel capacity: 500 kg * Maximum fuel capacity: 805 kg * Max wing loading: 154 kg/m² * Max power loading: 0.41 kg/kgp".
- Yakovlev_Yak-32 moreGeneral "Basic fuel capacity: 500 kg * Maximum fuel capacity: 805 kg * Max wing loading: 154 kg/m² * Max power loading: 0.41 kg/kgp".
- Yakovlev_Yak-8 moreGeneral "*Fuel/oil:".
- Zlin_Z-25_Šohaj moreGeneral "*Wing loading: 23.20 kg/m2".