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  2. Teledyne CAE J69 - Wikipedia

    en.wikipedia.org/wiki/Teledyne_CAE_J69

    Model 352 Model 352A Model 352-5a (CJ69-T-1025) 1,025 lbf (4.56 kN) thrust Model 354-12 ... The History of North American Small Gas Turbine Aircraft Engines ...

  3. General Electric CF34 - Wikipedia

    en.wikipedia.org/wiki/General_Electric_CF34

    The original engine contained a single stage fan driven by a 4-stage low pressure (LP) turbine, supercharging a 14-stage high pressure (HP) compressor driven by a 2-stage HP turbine, with an annular combustor. Later higher thrust versions of the CF34 feature an advanced technology core, with only 10 HP compressor stages.

  4. Power Jets WU - Wikipedia

    en.wikipedia.org/wiki/Power_Jets_WU

    A significantly different, symmetrical design was adopted for the second model. Ten spiral ducts connected the compressor outlet to a single, large, reverse-flow combustion chamber, the outlet of which discharged forward through the turbine before turning rearwards to exhaust through ten jet pipes.

  5. General Electric J85 - Wikipedia

    en.wikipedia.org/wiki/General_Electric_J85

    The J85 was originally designed to power a large decoy missile, the McDonnell ADM-20 Quail.The Quail was designed to be released from a B-52 Stratofortress in-flight and fly for long distances in formation with the launch aircraft, multiplying the number of targets facing the SA-2 surface-to-air missile operators on the ground.

  6. Jet engine - Wikipedia

    en.wikipedia.org/wiki/Jet_engine

    If aircraft performance were to increase beyond such a barrier, a different propulsion mechanism was necessary. This was the motivation behind the development of the gas turbine engine, the most common form of jet engine. The key to a practical jet engine was the gas turbine, extracting power from the engine itself to drive the compressor.

  7. Teledyne CAE J402 - Wikipedia

    en.wikipedia.org/wiki/Teledyne_CAE_J402

    The Teledyne CAE J402 is an American small turbojet engine. Several variants have been developed to power unmanned air vehicles such as missiles and target drones. Developed in the 1970s for the Harpoon anti-ship missile, the J402 was the first jet engine to be designed as a "wooden round", meaning that the engine had to be able to sit for long periods without maintenance or inspection and ...

  8. Pratt & Whitney J75 - Wikipedia

    en.wikipedia.org/wiki/Pratt_&_Whitney_J75

    The Pratt & Whitney J75 (civilian designation: JT4A) is an axial-flow turbojet engine first flown in 1955. A two-spool design in the 17,000 lbf (76 kN) thrust class, the J75 was essentially the bigger brother of the Pratt & Whitney J57 (JT3C).

  9. Boeing T50 - Wikipedia

    en.wikipedia.org/wiki/Boeing_T50

    The Boeing T50 (company designation Model 502) was a small turboshaft engine produced by Boeing. It was the first turboshaft engine to ever power a helicopter: a modified Kaman K-225 in 1951. [ 1 ] Based on Boeing's earlier Model 500 gas generator, the T50's main application was in the QH-50 DASH helicopter drone of the 1950s.

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