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  2. Bede BD-5 - Wikipedia

    en.wikipedia.org/wiki/Bede_BD-5

    "Bud Light Jet" BD-5J at Fargo 1997 BD-5J from Octopussy. While the new Hirth engine was being tested, Bede decided to create a variant of the BD-5 with a small jet engine. The result was the sleek BD-5J (also known as the "Acrostar Jet" [33]), a 300 mph (260 kn; 480 km/h) aircraft.

  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 Canada PW600 - Wikipedia

    en.wikipedia.org/wiki/Pratt_&_Whitney_Canada_PW600

    The Pratt & Whitney Canada PW600 series is a family of small turbofan engines developed by Pratt & Whitney Canada producing between 950 and 1,615 lbf (4.23 and 7.18 kN) of thrust and powering the Eclipse 500/550, the Cessna Citation Mustang and the Embraer Phenom 100.

  5. 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).

  6. Williams FJ44 - Wikipedia

    en.wikipedia.org/wiki/Williams_FJ44

    The Williams FJ44 is a family of small, two-spool, turbofan engines produced by Williams International for the light business jet market. Until the recent boom in the very light jet market, the FJ44 was one of the smallest turbofans available for civilian applications.

  7. Microturbo TRI 60 - Wikipedia

    en.wikipedia.org/wiki/Microturbo_TRI_60

    The TRI 60 engine was developed in the 1970s to meet the need for a small, inexpensive, reliable, and expendable jet engine for use in cruise missiles and other small unmanned air vehicles. This need was broken down into the key requirements for high production at low cost and a high thrust-to-weight ratio. [2]