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- Rolls-Royce_RB.203_Trent abstract "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.The RB.203 was a private venture engine based around the core of the Rolls-Royce Turbomeca Adour turbofan used in the SEPECAT Jaguar and the later Hawker Siddeley Hawk.The RB.203, the first three-spool engine, was intended as a civilian replacement for the earlier Rolls-Royce Spey.".
- Rolls-Royce_RB.203_Trent wikiPageID "34443371".
- Rolls-Royce_RB.203_Trent wikiPageRevisionID "578574672".
- Rolls-Royce_RB.203_Trent aircon "300".
- Rolls-Royce_RB.203_Trent bypass "3".
- Rolls-Royce_RB.203_Trent combustion "Annular chambers".
- Rolls-Royce_RB.203_Trent compression "16".
- Rolls-Royce_RB.203_Trent compressor "Single-stage fan, four-stage intermediate pressure, five-stage high pressure".
- Rolls-Royce_RB.203_Trent diameter "38.7".
- Rolls-Royce_RB.203_Trent firstRun "December".
- Rolls-Royce_RB.203_Trent hasPhotoCollection Rolls-Royce_RB.203_Trent.
- Rolls-Royce_RB.203_Trent length "82.2".
- Rolls-Royce_RB.203_Trent lists "*List of aircraft engines".
- Rolls-Royce_RB.203_Trent majorApplications Fairchild_228.
- Rolls-Royce_RB.203_Trent majorApplications "Convair 660".
- Rolls-Royce_RB.203_Trent majorApplications "Hawker Siddeley HS.136".
- Rolls-Royce_RB.203_Trent manufacturer Rolls-Royce_Limited.
- Rolls-Royce_RB.203_Trent ref "Flight International.".
- Rolls-Royce_RB.203_Trent similarEngines "*Rolls-Royce/SNECMA M45H".
- Rolls-Royce_RB.203_Trent thrust "16000.0".
- Rolls-Royce_RB.203_Trent weight "5.55".
- Rolls-Royce_RB.203_Trent turbine "Single-stage high pressure, single-stage intermediate, two-stage low pressure".
- Rolls-Royce_RB.203_Trent type Turbofan.
- Rolls-Royce_RB.203_Trent type "Three-spool medium bypass turbofan".
- Rolls-Royce_RB.203_Trent weight "1751.0".
- Rolls-Royce_RB.203_Trent subject Category:Medium-bypass_turbofan_engines.
- Rolls-Royce_RB.203_Trent subject Category:Rolls-Royce_aircraft_gas_turbine_engines.
- Rolls-Royce_RB.203_Trent subject Category:Turbofan_engines_1960–1969.
- Rolls-Royce_RB.203_Trent comment "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.The RB.203 was a private venture engine based around the core of the Rolls-Royce Turbomeca Adour turbofan used in the SEPECAT Jaguar and the later Hawker Siddeley Hawk.The RB.203, the first three-spool engine, was intended as a civilian replacement for the earlier Rolls-Royce Spey.".
- Rolls-Royce_RB.203_Trent label "Rolls-Royce RB.203 Trent".
- Rolls-Royce_RB.203_Trent sameAs m.0h_cm1n.
- Rolls-Royce_RB.203_Trent sameAs Q7361337.
- Rolls-Royce_RB.203_Trent sameAs Q7361337.
- Rolls-Royce_RB.203_Trent wasDerivedFrom Rolls-Royce_RB.203_Trent?oldid=578574672.
- Rolls-Royce_RB.203_Trent isPrimaryTopicOf Rolls-Royce_RB.203_Trent.