A manned Mars program made up of six missions is evaluated to determine the impact of using lunar liquid oxygen (LOX) as a propellant. Two departure and return nodes, low Earth orbit and low lunar orbit, are considered, as well as two return vehicle configurations, a full 70,000-kg vehicle and a 6800-kg capsule. The cost of lunar LOX delivered to orbit is expressed as a ratio of Earth launch cost.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Impact of Lunar Oxygen Production on Direct Manned MARS Missions


    Beteiligte:
    R. M. Young (Autor:in) / W. B. Tucker (Autor:in)

    Erscheinungsdatum :

    1992


    Format / Umfang :

    6 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Impact of lunar oxygen production on direct manned Mars missions

    Young, Roy M., Jr. / Tucker, William B. | NTRS | 1992



    MANNED MARS MISSIONS

    Online Contents | 1997


    Use of Lunar Produced Propellants for Manned Mars Missions

    Gus R Babb / William R Stump | NTRS | 1986


    Aerothermodynamics of manned Mars missions

    Park, Chul / Davies, Carol B. | NTRS | 1989