Potential role is examined emphasizing identification of mission capabilities for providing logistic support; electrical engine and nuclear mechanical power conversion system experience is projected to 1 to 10 Mw range to identify expected system characteristics; thermal arc and ion engines are considered; basic mission profile and typical trajectory characteristics; parametric mission performance characteristics for one-way, round-trip, and multi-trip missions; data indicate interrelationships between gross weight, power rating, specific impulse, and total propulsion time and their effect on payload capabilities.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Electrical propulsion capabilities for lunar exploration


    Weitere Titelangaben:

    AIAA J


    Beteiligte:
    Brown, H. (Autor:in) / Nicoll, Jr., H.E. (Autor:in)

    Erschienen in:

    AIAA Journal ; 1 , n 2


    Erscheinungsdatum :

    1963


    Format / Umfang :

    6 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    ELECTRICAL PROPULSION CAPABILITIES FOR LUNAR EXPLORATION

    BROWN, H. / NICOLL, H. E. | AIAA | 1963


    Propulsion capabilities for lunar mission

    Lee, Y.C. / Karen, B. | Engineering Index Backfile | 1961



    Nuclear Propulsion for Sustainable Lunar Exploration

    Bulman, M. / Borowski, S. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2006