The General Electric/Rolls-Royce F136 was an afterburning turbofan developed by General Electric, the Allison Engine Company and Rolls-Royce as an alternative powerplant to the Pratt and Whitney F135 for the Lockheed Martin F-35 Lightning II. It derived from the General Electric YF120, with hot section development by Allison and fan development by Rolls-Royce, and the GE Rolls-Royce Fighter Engine Team formed in 2002 split the work 60 percent General Electric and 40 percent Rolls-Royce. Full engine runs began on 21 July 2004, and the engine produced 28,000 lbf (125 kN) dry and 43,000 lbf (191 kN) with afterburner. The partners stopped work in December 2011 after failing to gather Pentagon support for further development.
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Source General Electric/Rolls-Royce F136 (Wikipedia)
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Source General Electric/Rolls-Royce F136 (Wikipedia)LeadQuote, Lead
developed by General Electric, Allison Engine Company, and Rolls-Royce
Also in Business Atlas: the manufacturer of this subject.
Source General Electric/Rolls-Royce F136 (Wikipedia)LeadQuote, Lead
developed by General Electric, Allison Engine Company, and Rolls-Royce
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1. General Electric/Rolls-Royce F136 (Wikipedia)
Development
On 21 July 2004, the F136 began full engine runs at GE
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developed by General Electric, Allison Engine Company, and Rolls-Royce
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