Designed to be reliable, simple, and rugged, basic components of engine are tubular-wall thrust chamber, direct-drive turbopump, gas generator, and controls; F-1 engine weighs 17,500 lb; development test program and design modification; gas generator and controls; Saturn C-1 booster with 8 Rocketdyne H-1 engines is applicable to clustering of 5 F-1's that will produce 7.5 million lb of thrust for Saturn C-5 vehicle; clustering problems now being solved. (See also Missiles and Space v 8 n 4 Oct 1962 p 26-8)


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    Titel :

    F-1 rocket engine development


    Weitere Titelangaben:

    Can Aeronautics Space J


    Beteiligte:
    Aldrich, D.E. (Autor:in) / Sanchini, D.J. (Autor:in)


    Erscheinungsdatum :

    1962


    Format / Umfang :

    7 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Rocket engine development

    Engineering Index Backfile | 1965


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    Butler, Kathleen N. | Online Contents | 1993


    Ion Rocket Engine Development

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    BMW Rocket Engine Development

    D. Singelmann / H. Mueller | NTIS | 1948