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Rolls-Royce LiftSystem

Aircraft Engines

The Rolls-Royce LiftSystem is the vertical lift part of the propulsion system of the F-35B, the short takeoff and vertical landing variant of the Lockheed Martin F-35 Lightning II. Together with the Pratt and Whitney F135 engine it forms the Integrated Lift Fan Propulsion System, which was awarded the Collier Trophy in 2001. Instead of separate lift engines or rotating bypass nozzles as on the Harrier, it combines a shaft-driven LiftFan, designed by Lockheed Martin and developed by Rolls-Royce, with a three-bearing swivel module that turns the exhaust nozzle downward and two roll posts that use engine bypass air for lateral control. Rolls-Royce managed the overall development and integration programme in Bristol, and the X-35B demonstrator flew with it in 2001.

Facts
Year
2001 1
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Source Rolls-Royce LiftSystem (Wikipedia)
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Source Rolls-Royce LiftSystem (Wikipedia)Design and development
Quote, Design and development
Rolls-Royce managed the overall development and integration program in Bristol, UK
Sources
1. Rolls-Royce LiftSystem (Wikipedia)
  • Design and development, Testing
    LiftSystem flight testing commenced in June 2001
  • Design and development
    Rolls-Royce managed the overall development and integration program in Bristol, UK
  • Of Make: Rolls-Royce, Lead
    The Rolls-Royce LiftSystem, together with the F135 engine, is an aircraft propulsion system designed for use in the STOVL variant of the F-35 Lightning II.
  • Part Of: Lockheed Martin F-35 Lightning II, Lead
    The Rolls-Royce LiftSystem, together with the F135 engine, is an aircraft propulsion system designed for use in the STOVL variant of the F-35 Lightning II.
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