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  2. General Electric TF34 - Wikipedia

    en.wikipedia.org/wiki/General_Electric_TF34

    Initial variant for Lockheed S-3, entered production in August 1972. TF34-GE-100. Variant for Fairchild A-10A, first flown in A-10 during May 1972. Production began in October 1974. TF34-GE-400A. Improved version of GE-2 for Lockheed S-3.

  3. General Electric CF34 - Wikipedia

    en.wikipedia.org/wiki/General_Electric_CF34

    Later higher thrust versions of the CF34 feature an advanced technology core, with only 10 HP compressor stages. Latest variants, the -10A and -10E , were derived from the CFM56 engine family, [ citation needed ] and have a radically different HP spool, containing a 9-stage compressor driven by a single stage turbine.

  4. Mikulin AM-34 - Wikipedia

    en.wikipedia.org/wiki/Mikulin_AM-34

    Rated at 800 PS (790 hp; 590 kW) with a weight of 864 kg (1,905 lb). GAM-34F A boosted version of the GM-34 it had bronze main bushings and used the crankshaft, block, heads, and some other components of the AM-34FRNV aircraft engine. Rated at 1,000 PS (990 hp; 740 kW) with a weight of 1,080 kg (2,380 lb) with a compression ratio of 7.3:1.

  5. Ford Cyclone engine - Wikipedia

    en.wikipedia.org/wiki/Ford_Cyclone_engine

    The 3.7 L's additional displacement comes from an increase in bore diameter to 95.5 mm (3.76 in), stroke remains identical to the 3.5 L at 86.7 mm (3.41 in). Ford Power Products sells this engine as the CSG-637 for industrial uses starting in mid-2015, which replaced the 4.2L Essex and is manufactured under license by Engine Distributors Inc. [ 5 ]

  6. British Aerospace ATP - Wikipedia

    en.wikipedia.org/wiki/British_Aerospace_ATP

    The ATP was developed during the 1980s, events such as such as the 1979 oil crisis and increasing public concern regarding aircraft noise led business planners at British Aerospace to believe that there was a market for a short-range, low-noise, fuel-efficient turboprop aircraft.

  7. Hirth F-33 - Wikipedia

    en.wikipedia.org/wiki/Hirth_F-33

    Data from Recreational Power Engineering General characteristics Type: Single cylinder, two-stroke, aircraft engine Bore: 76 mm (3.0 in) Stroke: 69 mm (2.7 in) Displacement: 313 cc (19.1 cu in) Length: 300 mm (11.8 in) Width: 299.5 mm (11.8 in) Height: 380 mm (15.0 in) Dry weight: 31 lb (14.1 kg) (base weight) 45 lb (20.4 kg) (with electric start and reduction drive) Components Valvetrain ...

  8. Type 63 anti-aircraft gun - Wikipedia

    en.wikipedia.org/wiki/Type_63_anti-aircraft_gun

    [3] The Type 65 retained the hull from the T-34-85 but the turret was replaced by an open-top box turret armed with twin Type 61 37mm anti-aircraft guns. [1] [2] The guns were loaded manually with 5-round clips.

  9. Management Component Transport Protocol - Wikipedia

    en.wikipedia.org/wiki/Management_Component...

    Management Component Transport Protocol (MCTP) is a protocol designed by the Distributed Management Task Force (DMTF) to support communications between different intelligent hardware components that make up a platform management subsystem, providing monitoring and control functions inside a managed computer system.