Propellant production on moon is proposed to eliminate payload propellant from earth takeoff weight; 10,000-lb payload can be landed on moon by 3,500,000-lb vehicle; propellant manufactured on moon can then be added to give 30,000-lb return vehicle 9200 fps velocity capability required for its trip to earth; total mission weight would be 3,530,000 lb; if no lunar propellant were available, it would be 10,000,000 lb; requirements for lunar propellant plant and possible equipment, e.g., rock crusher mining and locomotion equipment and equipment for processing and storage, and housing.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Propellant production on moon


    Weitere Titelangaben:

    Space/Aeronautics


    Beteiligte:
    Segal, H.M. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1963


    Format / Umfang :

    3 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Architectural Studies for the Production of Propellant on the Moon: Lunar Production Plant

    Diaz, J. / Duke, M. B. / American Society of Civil Engineers | British Library Conference Proceedings | 2004



    Thermal aspects of long-term propellant storage on moon

    Buna, T. | Engineering Index Backfile | 1964