Turbojets delivering more than 9000 lb of thrust will require starting power in excess of 100 hp for 20-sec start, and in excess of 1000 hp for 3-sec start; need for self contained starter system coupled with these high power requirements has led to development of air starters and cartridge starters. (see also Tech Data Digest v 16 n 2 Feb 1951 p 14-8; Aviation Week v 54 n 4 Jan 22 1951 p 22-7)


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    Titel :

    Starters for turbojet engines


    Weitere Titelangaben:

    Soc Automotive Engrs -- J


    Beteiligte:
    Downs, W.D. (Autor:in)


    Erscheinungsdatum :

    1951


    Format / Umfang :

    4 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch




    Starters For Turbojet Engines

    DOWNS, WILLIAM D. | SAE Technical Papers | 1951


    STARTERS FOR DIESEL ENGINES

    Lansing, R. P. | SAE Technical Papers | 1934


    Starters for airplane engines

    Allen, J.W. | Engineering Index Backfile | 1929


    STARTERS FOR GAS ENGINES

    FITZGERALD, J. W. | SAE Technical Papers | 1912


    J79 Turbojet Engines

    E. W. Lindner | NTIS | 1959