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Rolls-Royce RB.203 Trent : ウィキペディア英語版 | Rolls-Royce RB.203 Trent
The Rolls-Royce RB.203 Trent was a British medium-bypass turbofan engine of around 10,000lb thrust designed for production in the late 1960s, bearing no relation to the earlier Rolls-Royce RB.50 Trent turboprop or the later high bypass Rolls-Royce Trent turbofan.〔(''Flight International'' - RB.203 Trent ) www.flightglobal.com Retrieved: 23 January 2011〕 The RB.203 was a private venture engine built on the core of the Rolls-Royce Turbomeca Adour turbofan used in the SEPECAT Jaguar and the later Hawker Siddeley Hawk.〔(Commercial Aircraft Survey ), Flight Global, 23 November 1967, retrieved 28 January 2012〕 The RB.203, the first three-spool engine, was intended as a civilian replacement for the earlier Rolls-Royce Spey.〔(Aero Engines 1968, A "Flight" special review )〕 ==Specifications==
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