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  2. Rockwell X-30 - Wikipedia

    en.wikipedia.org/wiki/Rockwell_X-30

    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]

  3. List of Air Ministry specifications - Wikipedia

    en.wikipedia.org/wiki/List_of_Air_Ministry...

    The names of the aircraft shown in the table are not necessarily those they carried when provided for evaluation as at this point an aircraft would usually be referred to as the Manufacturer X.XX/XX, e.g., the Avro B.35/46 – this is in addition to the manufacturer's own separate internal designation for the aircraft, e.g., Avro 698.

  4. List of aircraft engines - Wikipedia

    en.wikipedia.org/wiki/List_of_aircraft_engines

    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 ...

  5. X engine - Wikipedia

    en.wikipedia.org/wiki/X_engine

    X-engine according to US Patent 1889583 (Eingetragen 1928) [1] Symmetrical X-Engine (90°/90°/90°/90°) An X engine is a piston engine with four banks of cylinders around a common crankshaft, such that the cylinders form an "X" shape when viewed front-on. The advantage of an X engine is that it is shorter than a V engine of the same number of ...

  6. Hirth 2704 - Wikipedia

    en.wikipedia.org/wiki/Hirth_2704

    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 ...

  7. Williams FJ33 - Wikipedia

    en.wikipedia.org/wiki/Williams_FJ33

    The Williams FJ33 is an American family of turbofan jet engines intended for use in very light jet aircraft. The FJ33 is a scaled-down version of the FJ44 engine. The FJ33-5A is the latest version certified in June 2016.

  8. Rockwell-MBB X-31 - Wikipedia

    en.wikipedia.org/wiki/Rockwell-MBB_X-31

    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 ...

  9. CAMit 3300 - Wikipedia

    en.wikipedia.org/wiki/CAMit_3300

    The CAMit 3300 is an Australian lightweight four-stroke, 6-cylinder, horizontally-opposed air-cooled aircraft engine.Direct drive and using a solid-lifter valvetrain, the 3300 develops 127 hp (95 kW) at 3300rpm.