Study of propulsion requirements for lunar orbiting and landing missions, including requirements imposed by flight paths, accelerometer errors, altitude determination errors, and impulse errors, with attention to minimizing number of maneuvers, number of engines, and throttling requirements; single fixed-thrust engine will satisfy requirements for orbiting mission; for landing from lunar orbit, single regeneratively cooled engine with throttling range as low as 3.5 to 1 appears acceptable; if system has separate landing engine, throttling range as low as 2 to 1 appears acceptable.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Spacecraft propulsion requirements for lunar missions


    Weitere Titelangaben:

    J Spacecraft Rockets


    Beteiligte:

    Erschienen in:

    Erscheinungsdatum :

    1965


    Format / Umfang :

    8 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :