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  2. Teledyne CAE J69 - Wikipedia

    en.wikipedia.org/wiki/Teledyne_CAE_J69

    Teledyne-Continental J69 turbojet at the Museum of Aviation, Warner Robins, Georgia: Type Turbojet: National origin: France/United States: Manufacturer Continental Aviation and Engineering / Teledyne CAE: Major applications: BQM-34 Firebee T-37 Tweet Ryan Model 147: Developed from: Turbomeca Marboré

  3. 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 ...

  4. Pratt & Whitney JT8D - Wikipedia

    en.wikipedia.org/wiki/Pratt_&_Whitney_JT8D

    It was a modification of the Pratt & Whitney J52 turbojet engine which powered the US Navy A-6 Intruder and A-4 Skyhawk attack aircraft. Eight models comprise the JT8D standard engine family, covering the thrust range from 12,250 to 17,400 pounds-force (54 to 77 kN), and power the 727, 737-100/200, and DC-9.

  5. Westinghouse J30 - Wikipedia

    en.wikipedia.org/wiki/Westinghouse_J30

    The Westinghouse J30, initially known as the Westinghouse 19XB, was a turbojet engine developed by Westinghouse Electric Corporation.It was the first American-designed turbojet to run, and only the second axial-flow turbojet to run outside Germany (after the British Metropolitan-Vickers F.2).

  6. 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).

  7. Westinghouse J34 - Wikipedia

    en.wikipedia.org/wiki/Westinghouse_J34

    The Westinghouse J34, company designation Westinghouse 24C, was a turbojet engine developed by Westinghouse Aviation Gas Turbine Division in the late 1940s. Essentially an enlarged version of the earlier Westinghouse J30, the J34 produced 3,000 pounds of thrust, twice as much as the J30.

  8. General Electric J85 - Wikipedia

    en.wikipedia.org/wiki/General_Electric_J85

    The General Electric J85 is a small single-shaft turbojet engine. Military versions produce up to 3,500 lb f (16 kN) of thrust dry; afterburning variants can reach up to 5,000 lb f (22 kN). The engine, depending upon additional equipment and specific model, weighs from 300 to 500 pounds (140 to 230 kg).

  9. Snecma Atar - Wikipedia

    en.wikipedia.org/wiki/SNECMA_Atar

    Early models were 2.85 m long, 0.9 m in diameter, and weighed 850 kg, while The C models and on were 3.68 m long including the long extension, 0.89 m in diameter, and weighed 940 kg. Later versions were generally similar to the C model, although the inclusion of the afterburner increased length to 5.23 m, and weights varied from 925 to 1,240 kg ...