Account of design background to P.1127V/STOL strike fighter and its BS.53 vectored thrust power plant; Pegasus engine is turbofan in which major part of fan delivery air is ducted through 2 outlets situated on either side of engine while remainder of air is passed through h-p compressor, combustion chamber and turbines before exhausting through 2 nozzles at rear of engine; performance and handling; operational characteristics of aircraft are described.
Hawker P.1127/bristol siddeley Pegasus combination
Aircraft Eng
Aircraft Engineering ; 34 , n 406
1962
4 pages
Article (Journal)
English
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