Matches in DBpedia 2015-10 for { ?s <http://dbpedia.org/property/eng1Note> ?o }
- Douglas_Cloudster_II eng1Note "ref| states two Continental W-670 of equivalent rating.|group=nb".
- Douglas_Dolphin eng1Note "::or 2x Pratt & Whitney R-1340-96 Wasp engines ;".
- E-Genius eng1Note "at 2,000 rpm, max".
- Eta_(glider) eng1Note "approximately".
- EuroSport_Crossover eng1Note "for cruise".
- Eurocopter_EC135 eng1Note "or 2 x Pratt & Whitney Canada PW206B turboshaft engines rated at".
- Extra_EA-400 eng1Note "for takeoff, continuous".
- F_L_S_Z_Der_Kricket_DK-1 eng1Note "approximate power".
- Fahlin_SF-2_Plymocoupe eng1Note "with 2:1 reduction gearing".
- Fairey_FB-1_Gyrodyne eng1Note "at 3,000 rpm".
- Farner_HF_Colibri_1_SL eng1Note ", coupled to drive a single, foldable propeller".
- Fauvel_AV.2 eng1Note "at 2,300 rpm. Engine in pusher configuration.".
- Fiat_AN.1_(aircraft) eng1Note "maximum at 1,700 rpm".
- Fieseler_Fi_5 eng1Note "for take-off".
- Fliegende_Panzerfaust eng1Note "Total weight 150 kg".
- Focke-Wulf_Fw_300 eng1Note ":::or 4 x Daimler-Benz DB 603E inverted V-12 liquid-cooled piston engines".
- Focke-Wulf_Ta_254 eng1Note "with a three-speed two-stage intercooled supercharger, with MW 50 boost".
- Fokker_50 eng1Note ":::Fokker 60: 2x Pratt & Whitney Canada PW127B turboprop engines".
- Fokker_C.V eng1Note ":::C.V-D: 1 x Bristol Jupiter 9-cyl. air-cooled radial piston engine :::C.V-E: 1 x Napier Lion W-12-cyl. water-cooled piston engine ::::or 1 x Armstrong Siddeley Panther II 14-cyl. air-cooled radial piston engine ::::or 1 x Bristol Jupiter VI 9-cyl. air-cooled radial piston engine".
- Fokker_D.VII eng1Note "**or 1 × Mercedes D.IIIa 6-cyl. water-cooled in-line piston engine **or 1 × BMW IIIa 6-cyl. water-cooled in-line piston engine".
- Fokker_F.VIII eng1Note ":::2 x licence-built Gnome-Rhône Jupiter".
- Gabardini_G.9 eng1Note ":::G.9bis - 1 x Hispano-Suiza HS42 V-8 water-cooled piston engine".
- Gardan_GY-120 eng1Note "at 7,000 rpm, toothed belt 2.7:1 output speed reduction".
- Gee_Bee_Model_Z eng1Note "supercharged".
- General_Atomics_MQ-9_Reaper eng1Note "with Digital Electronic Engine Control".
- Gerner_G_II_R eng1Note "80.0".
- Gribovsky_G-15 eng1Note "approximately. Engine sub-type and exact power unknown.".
- Grumman_JF_Duck eng1Note ":::JF-1: 1 x Pratt & Whitney R-1830-62 :::JF-2: 1 x Pratt & Whitney R-1830-102 :::JF-3: 1 x Pratt & Whitney R-1830-80".
- Hannover_CL.III eng1Note "::or 1x Mercedes D.III".
- Hanriot_H.110 eng1Note "240000.0".
- Heinkel_He_176 eng1Note "50.0".
- Heinkel_Lerche eng1Note "*:or 2 × Daimler-Benz DB 603E V-12 liquid-cooled direct fuel-injected piston engines *:".
- Heinkel_Lerche eng1Note "2000.0".
- Hirth_Hi_20_MoSe eng1Note "at 5,500 rpm".
- Hispano_Aviación_HA-1112 eng1Note ":::HA-1112-M1L 1 x Rolls-Royce Merlin 500/45 V-12 liquid-cooled piston engine".
- Horten_H.III eng1Note "::::H.IIIe: 1 x Volkswagen engine".
- Hummel_Bird eng1Note "to".
- Junkers_F.13 eng1Note ":::F.13fe: 1 x Junkers L5 6-cyl. water-cooled in-line piston engine".
- Junkers_G.38 eng1Note "inboard".
- Junkers_Ju_287 eng1Note ":::Ju 287 V2 and Ju 287 V3: 6 x Junkers Jumo 004B-1".
- Kamov_Ka-8 eng1Note ":::licence built BMW motorcycle engine".
- Kawasaki_Ki-78 eng1Note "rated at with Water/Methanol injection for short durations".
- Kestrel_K-350 eng1Note "flat rated to".
- Keystone-Loening_Commuter eng1Note "-".
- Knapp_Lil_Cub eng1Note "modified".
- Landray_GL.02 eng1Note "with a six belt speed reducer".
- Latécoère_225 eng1Note "at 4,500 rpm".
- Latécoère_3 eng1Note ",".
- Latécoère_350 eng1Note "at 2,000 rpm at sea level".
- Latécoère_440 eng1Note "at 2,000 rpm".
- Latécoère_550 eng1Note "at 2,250 rpm".
- Lebouder_Autoplane eng1Note "only for use in aircraft mode".
- Letov_Š-33 eng1Note "built by Praga".
- Lightwing_Rooster eng1Note "engine optional".
- Lockheed_XV-4_Hummingbird eng1Note "take-off thrust".
- Loire-Nieuport_161 eng1Note "240000.0".
- Loire-Nieuport_LN.401 eng1Note "at".
- MFI_BA-12_Sländan eng1Note "at 4,200 rpm, reduced by 1.7:1 by toothed belt to propeller shaft".
- MacFam_Cavalier eng1Note "Can be built with engines in the 85hp-200hp range".
- Macchi_M.C.94 eng1Note "- Take-off rating".
- Macfie_monoplane eng1Note "225.0".
- Mansyū_Ki-98 eng1Note "** at ** at".
- Mansyū_Ki-98 eng1Note "for take-off".
- Martin_2-0-2 eng1Note ",".
- Martin_4-0-4 eng1Note ",".
- Mitsubishi_J4M eng1Note "::: at ::: at".
- Mitsubishi_J4M eng1Note "at take-off".
- Morane-Saulnier_MS.341 eng1Note "at 2,400 rpm".
- Myasishchev_M-50 eng1Note "wet".
- Myasishchev_M-55 eng1Note "::::M-17: 1x Kolesov RD-36-51".
- N500_Naviplane eng1Note "*Max continuous RPM: 14,500 *Fuel consumption: 247 Imp gal/engine/hour, fuel type: Kerosene JP4/TR4.".
- Nakajima_G10N eng1Note "::::Fugaku: 6x Nakajima NK11A 18-cyl. air-cooled radial piston engines developing at take-off".
- Nakajima_G10N eng1Note "at take-off".
- Nakajima_J1N eng1Note ":: at :: at :::J1N1: 1x Nakajima NK1F Sakae 21 + 1x Nakajima NK1F Sakae 22 handed engines".
- Nakajima_J1N eng1Note "take-off rating".
- Nippi_NP-100 eng1Note "at 6,000 rpm".
- Noorduyn_Norseman eng1Note "Power Loading 12.3 lb/hp".
- Northrop_AQM-35 eng1Note "::::Q-4B/AQM-35B: 1x General Electric J85-GE-5 turbojet, thrust".
- Northrop_Grumman_E-10_MC2A eng1Note ":::: or 2x General Electric CF6-80C".
- Northrop_N-9M eng1Note "2".
- PZL_P.11 eng1Note "or 1x Polish Skoda Works Mercury VI.S2 **P.11a - – Polish Skoda Works Mercury IV.S2 **P.11b – Gnome-Rhône 9K Mistral or I.A.R. 9K Mistral **P.11f – I.A.R. 9K Mistral **P.11g – P.Z.L. Mercury VIII".
- Pander_E eng1Note "continuous at 1,500 rpm and maximum 37 kW at 1,580 rpm".
- Percival_P.74 eng1Note "gas horse-power".
- Piaggio_P.7 eng1Note "0.7".
- Pocino_PJ.1A eng1Note "Rotax".
- Potez_506 eng1Note "at sea level. A supercharger turning at 10.92×engine speed maintained this power to . Output geared down 3:2. Compression ratio 7.25.".
- Potez_75 eng1Note "at take-off".
- Potez_XI eng1Note "with a Rateau turbo-charger".
- RAE_Scarab eng1Note "at 3,200 rpm".
- RFB_X-113 eng1Note "derated from".
- RWD_23 eng1Note "**or 1 x Avia 3 **or 1 x Blackburn Cirrus Minor".
- Radioplane_XKD4R eng1Note "530.0".
- Rotorvox_C2A eng1Note "continuous".
- Ryan_XV-5_Vertifan eng1Note "horizontal thrust, VTOL thrust from lift fans".
- SNCAC_NC.2001_Abeille eng1Note "take-off power".
- SNCAC_NC.3021_Belphégor eng1Note "at sea level".
- SNCAC_NC.510 eng1Note "180000.0".
- SNCAC_NC_211 eng1Note "at 2,600 rpm with Hg / + boost for take-off".
- SNCAO_700 eng1Note "LH rotation".
- SNCASE_SE-2100 eng1Note "30000.0".