Background and description of engine which was developed in 1954 as lightweight lift jet engine for Short SC.1 research aircraft; RB.145 was produced as development of RB.108 with additional compressor stage; summary of RB.108-powered rigs and aircraft flight testing; development is now concentrated on second-generation lift jet, RB. 162, which has initial thrust of 4400 lb and thrust-to-weight ratio of 16 to 1.
Rolls-Royce RB.108
Shell Aviation News
Shell Aviation News ; n 328
1965
5 pages
Aufsatz (Zeitschrift)
Englisch
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