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  2. PBS TJ100 - Wikipedia

    en.wikipedia.org/wiki/PBS_TJ100

    The TJ100 engine entered service in 2003, [1] and is the most popular of PBS's turbojet engines as more than 1,000 engines have been sold to 40 countries worldwide. [2] The engine has been developed for unmanned aerial vehicles , including target drones , remote carriers, unmanned combat aerial systems , light experimental jet aircraft , and ...

  3. Rolls-Royce Olympus - Wikipedia

    en.wikipedia.org/wiki/Rolls-Royce_Olympus

    The somewhat revised BOl.1/2B, ran in December 1951 producing 9,750 lbf (43.4 kN) thrust. [ 14 ] The engine was by now ready for air testing and the first flight engines, designated Olympus Mk 99, were fitted into a Canberra WD952 which first flew with these engines derated to 8,000 lbf (36 kN) thrust in August 1952.

  4. Williams FJ33 - Wikipedia

    en.wikipedia.org/wiki/Williams_FJ33

    The FJ33 has a dry weight of less than 300 lb (140 kg), overall diameter of 18.36 in (466 mm), 38.43 in (976 mm) overall length, and produces between 1,000 lbf (4,400 N) and 1,800 lbf (8,000 N) static thrust.

  5. Rolls-Royce Pegasus - Wikipedia

    en.wikipedia.org/wiki/Rolls-Royce_Pegasus

    A 2-stage LP turbine drove the fan. There was no plenum at fan exit, but 4 thrust-vectoring nozzles were fitted. Further development of the engine then proceeded in tandem with the aircraft, the Hawker P.1127. The aircraft first flew (tethered hover) on 21 October 1960, powered by the BE53/3 (Pegasus 2).

  6. Pratt & Whitney Canada PW800 - Wikipedia

    en.wikipedia.org/wiki/Pratt_&_Whitney_Canada_PW800

    After the Advanced Technology Fan Integrator demonstrator first ran on March 17, 2001, which became the PW1000G, Pratt & Whitney Canada was searching for a launch customer for the initially geared PW800, in the 10,000–19,000 lbf (44–85 kN) thrust range, bridging the gap between P&WC's PW300 and P&W's PW6000, intended for the regional- and ...

  7. Microturbo TRI 60 - Wikipedia

    en.wikipedia.org/wiki/Microturbo_TRI_60

    This variant is an uprated model of the 60-1 engines, with thrust increased to 3.7 kN (830 lbf). [2] TRI 60-2 071: This model powers the Aerospatiale C.22 target drone, and is slight uprated to 4.0 kN (900 lbf). TRI 60-2 074: This model powers several versions of the MQM-107 Streaker drone. TRI 60-2 077: This model powers the RBS-15 anti-ship ...

  8. Eurojet EJ200 - Wikipedia

    en.wikipedia.org/wiki/Eurojet_EJ200

    EJ200 displayed at ILA Berlin Air Show 2018. The Eurojet consortium was formed in 1986 to co-ordinate and manage the project largely based on XG-40 technology. In common with the XG-40, the EJ200 has a three-stage fan with a high pressure ratio, five-stage low-aspect-ratio high-pressure (HP) compressor, a combustor using advanced cooling and thermal protection, and single-stage HP and LP ...

  9. General Electric CF700 - Wikipedia

    en.wikipedia.org/wiki/General_Electric_CF700

    CF700-2B Baseline aft-fan CJ610 variant rated at 4,200 lbf (19,000 N) for take-off CF700-2V The 2B modified for continuous vertical operation on the Lunar Landing Research Vehicle (LLRV) and Lunar Landing Training Vehicle (LLTV)