Design and development of pressure-fed, sixteen-engine, bipropellant reaction control system for Apollo Lunar Module; design requirements, from which basic configuration evolved, as well as detailed system description are presented; overall development program is outlined and principal development problems and solutions are discussed; significant ground test techniques and results are summarized; highlights of system assembly and checkout are described. (31690)


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    Titel :

    Apollo Lunar Module control system


    Weitere Titelangaben:

    ASME Aviation Space -- Progress Prospects


    Beteiligte:
    Grossman, R.L. (Autor:in) / Hagerman, R.H. (Autor:in) / Williams, O.S. (Autor:in)

    Kongress:

    ASME Annual Aviation and Space Conference ; 1968 ; United States , Beverly Hills, CA Control



    Erscheinungsdatum :

    1968


    Format / Umfang :

    11 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    The Apollo Lunar Module Reaction Control System.

    Grossman, R. L. / Hagerman, R. H. / Williams, O. S. | NTRS | 1968


    The Apollo Lunar Module

    Ford, T.E. | Emerald Group Publishing | 1969


    Apollo experience report: Lunar module reaction control system

    Vaughan, C. A. / Villemarette, R. / Karakulko, W. et al. | NTRS | 1972


    APOLLO Experience Report Lunar Module Reaction Control System

    C. A. Vaughan / R. Villemarette / W. Karakulko et al. | NTIS | 1972


    Apollo Lunar Module Landing Gear

    Rogers, W. F. | NTRS | 1972