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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. Pratt & Whitney Canada PW300 - Wikipedia

    en.wikipedia.org/wiki/Pratt_&_Whitney_Canada_PW300

    The PW 300 series has been developed in partnership with MTU who are responsible for the low pressure turbine. The first variant, the PW305A, has the following configuration and was designed with a core flexible enough for engines with take-off thrusts from 20 kN to 31 kN (4,500 to 7,000 lb): a single-stage fan driven by a three-stage low pressure turbine, supercharging a four-stage axial ...

  4. 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 ...

  5. 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.

  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 TRS 18 - Wikipedia

    en.wikipedia.org/wiki/Microturbo_TRS_18

    Includes an engine driven alternator and fuel and oil lubrication pumps. Dry weight as 18-046. Take-off thrust increased to 1.15 kN (260 lb st) and maximum continuous thrust to 1.10 kN (247 lb st). TRS 18-076 Intended for the Meteor-Mirach 100. Includes an engine driven alternator and fuel and oil lubrication pumps. Dry weight as 18-046.

  8. PBS TJ150 - Wikipedia

    en.wikipedia.org/wiki/PBS_TJ150

    The engine has a built-in starter-generator to start and supply power to the deck network, and a separate oil system. The PBS TJ150 engine was developed from PBS TJ100 engine utilizing the same outer diameter dimensions and engine weight but has 20% more power. One of the PBS TJ150 engine versions enables landing on salt water. [4]

  9. Volvo RM12 - Wikipedia

    en.wikipedia.org/wiki/Volvo_RM12

    Produced by Volvo Aero, the RM12 is a derivative of the General Electric F404J. The fan was completely redesigned with thickened first stage blades which deform (causing the thrust loss) but do not fracture or cause downstream damage to pass more flow for higher thrust and to be more tolerant of a bird-strike.

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