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searching for Gnome et Rhône 47 found (134 total)

Hopfner HV-4/28 (221 words) [view diff] exact match in snippet view article find links to article

refurbishment that included a change or powerplant from the original Heiro to a Gnome et Rhône 9A Jupiter engine and was sold to a private owner under the new designation

FBA 17 (1,037 words) [view diff] exact match in snippet view article find links to article

172 HE.2 2-seat trainer, Gnome et Rhône 5B-powered, (5 built). 172 HMT.2 2-seat amphibious transport aircraft, Gnome et Rhône 5B-powered, (1 built). 172

Farman F.150 (296 words) [view diff] exact match in snippet view article find links to article

production. F.150 The original B.3 version powered by 2x 280 kW (380 hp) Gnome et Rhône 9Aa 9-cylinder radial piston engines, of which only one was built. F

Latécoère 21 (264 words) [view diff] exact match in snippet view article find links to article

side in separate open cockpits. Latécoère 21 - initial version with Gnome et Rhône 9A Jupiter engines (1 built) Latécoère 21bis - main production version

Blériot-SPAD S.51 (564 words) [view diff] exact match in snippet view article find links to article

1x 280 kW (380 hp) Gnome et Rhône 9Aa radial engine. S.51/2 Refined version exported to Poland, 1x 310 kW (420 hp) Gnome et Rhône 9Ab radial engine. S

Farman F.190 (1,105 words) [view diff] exact match in snippet view article find links to article

version with a 170 kW (230 hp) Gnome et Rhône 5Ba engine, 57 built. F.191 Powered by a 180 kW (240 hp) Gnome et Rhône 5Bc for long distance flying, one

Farman F.300 (1,486 words) [view diff] exact match in snippet view article find links to article

with Gnome et Rhône 5Ba engines (six built) F.304 long-range version with Lorraine 9N engines (one built) F.305 production version with Gnome et Rhône 9A

Villiers 31 (587 words) [view diff] exact match in snippet view article find links to article

welded without the use of a filler metal. There was a 310 kW (420 hp) Gnome et Rhône 9Ab nine-cylinder radial engine in the nose, which some photographs

Latham 43 (379 words) [view diff] exact match in snippet view article find links to article

Lorraine 12Da engines (2 built) production version for France with Gnome et Rhône 9Aa engines (18 built) production version for Poland with Lorraine engines

Tupolev ANT-43 (245 words) [view diff] exact match in snippet view article find links to article

General characteristics Crew: 1 Capacity: 6 passengers Powerplant: 1 × Gnome et Rhône 14Rsd 14-cylinder air-cooled radial piston engine, 600 kW (800 hp) "ANT-43 ::

Bratu 220 (436 words) [view diff] exact match in snippet view article find links to article

842 lb) Powerplant: 1 × Gnome et Rhône 9A 9-cyl. air-cooled radial piston engine, 310 kW (420 hp) Powerplant: 2 × Gnome et Rhône 5K Titan 5-cyl. air-cooled

Latécoère 6 (1,000 words) [view diff] exact match in snippet view article find links to article

aircraft to take four more modern and powerful engines, 420 hp (310 kW) Gnome et Rhône 9A Jupiter engines. This revised machine was known as the Latécoère

Levasseur PL.7 (801 words) [view diff] exact match in snippet view article find links to article

(for "transport") and promoted as an airliner. This was fitted with a Gnome et Rhône 9A Jupiter engine and had a revised fuselage with side-by-side seating

Junkers W 34 (1,613 words) [view diff] exact match in snippet view article find links to article

W 34 a 331 kW Gnome et Rhône 9A Jupiter engine, speed: 190 km/h, wingspan: 17.75 m and length 11.10 m W 34 be 375 kW Gnome et Rhône 9A Jupiter engine

CAMS 54 (1,222 words) [view diff] exact match in snippet view article find links to article

edge. These engines were much more powerful than the 280 kW (380 hp) Gnome et Rhône 9Aas of the CAMS 51 and to accommodate them and their propellers on

FBA 21 (459 words) [view diff] exact match in snippet view article find links to article

Lorraine 12Eb W-12 engine (2 built) 21/3 flying boat airliner with Gnome et Rhône 9Ab radial engine (1 converted from 21/1) 21/4 HT.3 amphibian mailplane

CWL WZ.X (706 words) [view diff] exact match in snippet view article find links to article

the prototype, with a fourth (WZ.X/IV) powered by a 400 kW (530 hp) Gnome et Rhône 9A Jupiter radial engine with four-blade propeller. The WZ.X did not

Loire 45 (362 words) [view diff] exact match in snippet view article find links to article

completed at Saint-Nazaire, equipped for comparison with a 14-cylinder Gnome et Rhône 14 Kd engine of 740 hp and armed with two 20mm Oerlikon guns in the

Bréguet 26T (410 words) [view diff] exact match in snippet view article find links to article

412 kg (3,113 lb) Gross weight: 3,055 kg (6,735 lb) Powerplant: 1 × Gnome et Rhône 9Ab nine-cylinder radial engine, 340 kW (450 hp) Performance Cruise

Kalinin K-6 (252 words) [view diff] exact match in snippet view article find links to article

capacity: 550 kg (1,210 lb) fuel; 50 kg (110 lb) oil Powerplant: 1 × Gnome et Rhône 9A Jupiter 9-cylinder air-cooled radial piston engine, 310 kW (420 hp)

Loire 70 (465 words) [view diff] exact match in snippet view article find links to article

tractors and one as a pusher. The original engines, three 500 hp (373 kW) Gnome et Rhône 9Kbr radials, were not powerful enough and were replaced with 740 hp

Farman F.120 (1,653 words) [view diff] exact match in snippet view article find links to article

123 with two 450 hp Hispano-Suiza 12Hb V12s, or F.124 with two 420 hp Gnome et Rhône 9Ad Jupiter radial engines. The Farman F.120 was a multi-engine multirole

Bernard 18 (352 words) [view diff] exact match in snippet view article find links to article

820 kg (4,010 lb) Gross weight: 2,700 kg (5,950 lb) Powerplant: 1 × Gnome et Rhône 9Ab air-cooled radial piston engine , 313 kW (420 hp) Performance Range:

Blanchard BB-1 (228 words) [view diff] exact match in snippet view article find links to article

(226.0 sq ft) Max takeoff weight: 1,280 kg (2,822 lb) Powerplant: 1 × Gnome et Rhône 9A Jupiter radial piston engine, 280 kW (380 hp) Propellers: 2-bladed

IVL Haukka (332 words) [view diff] exact match in snippet view article find links to article

940 kg (2,072 lb) Gross weight: 1,290 kg (2,844 lb) Powerplant: 1 × Gnome et Rhône 9Ac Jupiter 9-cylinder air-cooled radial piston engine, 309 kW (414 hp)

CAMS 51 (259 words) [view diff] exact match in snippet view article find links to article

150 kg (6,945 lb) Gross weight: 5,150 kg (11,354 lb) Powerplant: 2 × Gnome et Rhône 9Aa (licence-built Bristol Jupiter) , 283 kW (380 hp) each Performance

Latécoère 550 (967 words) [view diff] no match in snippet view article find links to article

flew the following year. It was a high-wing monoplane with its four Gnôme et Rhône 9 Kdr radial engines mounted on the wings in tandem, tractor-pusher

Farman F.70 (447 words) [view diff] exact match in snippet view article find links to article

12Fe V-12 piston engine. F.73 Variant re-engined with a 380hp (282kW) Gnome et Rhône 9Aa Jupiter radial piston engine. Brazil Brazilian Air Force France

CAMS 53 (416 words) [view diff] exact match in snippet view article find links to article

converted from 53 via 53-1) 53/3 - (redesignated to 56) - version with Gnome et Rhône 9A (licence-built Bristol Jupiter) engines (four built) 53/4 53/5 53R

Heinkel HE 5 (849 words) [view diff] exact match in snippet view article find links to article

prototype with Napier Lion engine (1 built) HE 5b - production version with Gnome et Rhône 9A Jupiter radial engine HE 5c - production version for Soviet Union

Lioré et Olivier LeO H-190 (1,733 words) [view diff] exact match in snippet view article find links to article

frames and fabric coverings. The flying boat was typically powered by a Gnome et Rhône 9Ad Jupiter air-cooled radial engine, capable of generating up to 420

Wibault 7 (919 words) [view diff] exact match in snippet view article find links to article

827 kg (1,823 lb) Gross weight: 1,444 kg (3,183 lb) Powerplant: 1 × Gnome et Rhône 9Ac , 313 kW (420 hp) Performance Maximum speed: 227 km/h (141 mph,

List of motorcycles in The Art of the Motorcycle exhibition (353 words) [view diff] exact match in snippet view article find links to article

0 cu in) 1932 France Y Y Dollar V4 748 cc (45.6 cu in) 1933 France Y Y Gnome et Rhône M1 306 cc (18.7 cu in) 1934 France Y Harley-Davidson Model E 61 cu in

Latécoère 17 (959 words) [view diff] exact match in snippet view article find links to article

converted from 17-3R. Latécoère 17-1J Version of 17-1R with 280 kW (380 hp) Gnome et Rhône 9A Jupiter engine. One built. Latécoère 17-3J Production version of

Focke-Wulf A 17 Möwe (471 words) [view diff] exact match in snippet view article find links to article

designated A 29. A 17 - Eight-passenger airliner powered by 420 hp (310 kW) Gnome et Rhône 9Aa Jupiter. One prototype and 11 production aircraft. A 17a - Conversion

Dyle et Bacalan DB-10 (786 words) [view diff] exact match in snippet view article find links to article

150 kg (6,945 lb) Gross weight: 5,600 kg (12,346 lb) Powerplant: 2 × Gnome et Rhône 9A Jupiter 9-cylinder radial, 360 kW (480 hp) each Propellers: 2-bladed

Nieuport-Delage NiD 50 HB.4 (240 words) [view diff] exact match in snippet view article find links to article

World's Aircraft 1928 General characteristics Crew: 4/5 Powerplant: 2 × Gnome et Rhône 9A Jupiter 9-cylinder air-cooled radial piston engines, 310 kW (420 hp)

Blackburn Type I (1,366 words) [view diff] exact match in snippet view article find links to article

weight: 950 lb (430 kg) Gross weight: 1,500 lb (680 kg) Powerplant: 1 × Gnome et Rhône 7 cylinder rotary , 80 hp (60 kW) Performance Maximum speed: 70 mph

Bernard 190 (910 words) [view diff] exact match in snippet view article find links to article

payload. 190T Single-engined airliner, powered by a 358 kW (480 hp) Gnome et Rhône 9Ady (licence-built Bristol Jupiter) radial piston engine. 191T A single

Lioré et Olivier LeO 20 (514 words) [view diff] exact match in snippet view article find links to article

(11,155 lb) Max takeoff weight: 5,600 kg (12,346 lb) Powerplant: 2 × Gnome et Rhône 9Ady Jupiter 9-cylinder air-cooled radial piston engine, 360 kW (480 hp)

Latécoère 28 (1,777 words) [view diff] exact match in snippet view article find links to article

3-I A passenger version of the 28.3, powered by a 700 hp (521.99 kW) Gnome et Rhône 14Kb Mistral Major radial engine, one built. Laté 28.4-I A development

Farman F.220 (1,594 words) [view diff] exact match in snippet view article find links to article

12Xirs engines (1 built) S.N.C.A.C. NC.223.2 - bomber version with Gnome et Rhône 14N engines (not built) S.N.C.A.C. NC.223.3 - bomber version with 910 hp

Farman F.60 Goliath (3,384 words) [view diff] exact match in snippet view article find links to article

900 kg (6,393 lb) Gross weight: 5,400 kg (11,905 lb) Powerplant: 2 × Gnome et Rhône 9A Jupiter 9-cylinder air-cooled radial piston engines, 340 kW (450 hp)

List of Schneider Trophy aircraft (377 words) [view diff] exact match in snippet view article find links to article

were run during 1924. 1924 n/a France Blanchard BB-1 280 kW (380 hp) Gnome et Rhône 9A Jupiter Withdrew before trials n/a 1924 n/a Great Britain Gloster

Gourdou-Leseurre GL.30 (1,215 words) [view diff] exact match in snippet view article find links to article

285 kg (628 lb) - (ca. 200 L (53 US gal; 44 imp gal)) Powerplant: 1 × Gnome et Rhône 9A Jupiter VIII 9-cyliner air-cooled radial piston engine, 450 kW (600 hp)

Renault 12Fe (1,034 words) [view diff] exact match in snippet view article find links to article

Renault (in French) (22) – via Safran. Laux, James M (March 1980). "Gnome et Rhône - An Aviation Engine Firm in the First World War: Le Rhône". Aerospace

Lioré et Olivier LeO 45 (4,605 words) [view diff] exact match in snippet view article find links to article

French) Notice descriptive et d'utilisation de l'avion LeO. 451 à moteurs Gnome et Rhône 14N, SNCASE, 1939 Wikimedia Commons has media related to Lioré et Olivier