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The X-30 configuration integrated engine and fuselage. The shovel-shaped forward fuselage generated a shock wave to compress air before it entered the engine. The aft fuselage formed an integrated nozzle to expand the exhaust. The engine between was a scramjet. At the time, [when?] no scramjet engine was close to operational. [citation needed]
B Bailey Bailey C-7-R "Bull's Eye" 1927 = 140 hp 7RA. Bailey Aviation Main article: Bailey Aviation Bailey B200 Bailey Hornet Bailey V5 engine Baradat–Esteve (Claudio Baradat Guillé & Carlos Esteve) Baradat toroidal engine Basse und Selve Main article: Basse und Selve Basse und Selve BuS. 120 hp (125 mm × 160 mm (4.9 in × 6.3 in) 120-130 hp) Basse und Selve BuS.III 150 hp Basse und Selve ...
The Lycoming XR-7755 was the largest piston aircraft engine ever built in the United States, [Note 1] with 36 cylinders totaling about 7,750 in 3 (127 L) of displacement and a power output of 5,000 horsepower (3,700 kilowatts).
The Pratt & Whitney R-4360 Wasp Major is an American 28-cylinder four-row radial piston aircraft engine designed and built during World War II.At 4,362.5 cu in (71.5 L), it is the largest-displacement aviation piston engine to be mass-produced in the United States, and at 4,300 hp (3,200 kW) the most powerful.
Prototypes and initial production, boost engines [citation needed] 19B Increased mass flow version delivering 1,400 lbf (6.23 kN) at 18,000 rpm at sea level, added gearbox to allow engine to be a prime driver [citation needed] 19XB-2B Company designation for WE-20. [2] XJ30-WE-7 1,600 lbf (7.1 kN) for Northrop X-4 [citation needed] XJ30-WE-8
The 2si 460 is a family of in-line twin-cylinder, two-stroke, single ignition, aircraft engines that were designed for ultralight aircraft. [1]The basic engine was originally designed and produced by ILO-Motorenwerke of Germany and was later acquired by the AMW Cuyuna Engine Company of Beaufort, South Carolina and marketed under the Cuyuna brand name.
The Rockwell-Messerschmitt-Bölkow-Blohm X-31 is an experimental jet aircraft designed to test fighter thrust vectoring technology. It was designed and built by Rockwell and Messerschmitt-Bölkow-Blohm (MBB), as part of a joint United States and German Enhanced Fighter Maneuverability program to provide additional control authority in pitch and yaw, for significantly more maneuverability than ...
Data from Recreational Power Engineering General characteristics Type: Twin cylinder, two-stroke, in-line, aircraft engine Bore: 76 mm (3.0 in) Stroke: 69 mm (2.7 in) Displacement: 625 cc (38.1 cu in) Length: 377 mm (14.8 in) Width: 450 mm (17.7 in) Height: 383 mm (15.1 in) Dry weight: 73 lb (33.1 kg) with free air cooling, 79 lb (35.8 kg) with fan cooling, including recoil starter and exhaust ...