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.


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    Titel :

    Rolls-Royce RB.108


    Weitere Titelangaben:

    Shell Aviation News


    Beteiligte:
    Davies, D.O. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1965


    Format / Umfang :

    5 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch




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