First medium power, straight jet engine for piloted aircraft consists of complete Mamba power plant with new front end substituted for reduction gear and propeller shaft of propeller turbine engine; 1000-lb thrust Adder has 10-stage, axial flow compressor; 2-stage turbine, of axial flow type, provides power to drive compressor and auxiliaries; max diam over auxiliaries 28 in.; oa length 73.3 in.; weight (dry) 550 lb.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Armstrong Siddeley's Adder turbojet


    Additional title:

    Aero Digest


    Contributors:

    Published in:

    Aero Digest ; 61 , n 4


    Publication date :

    1950


    Size :

    2 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




    Armstrong-Siddeley and Armstrong-Whitworth

    Engineering Index Backfile | 1934



    Armstrong-Siddeley and Armstrong-Whitworth

    Engineering Index Backfile | 1934


    TURBOJET AUTOMOBILE

    CHEN XIAOHUI | European Patent Office | 2018

    Free access

    Armstrong-siddeley

    Engineering Index Backfile | 1930