Booster requirements of interplanetary flight and analysis of trajectory data with respect to nuclear-propelled orbital launch vehicles; tabulation of attractive categories of nonstop round-trip flybys to Mars and Venus; types of planetary stopovers considered are Mars short and long stopover and Venus short stopover; application of nuclear-propelled orbital launch vehicles to such trajectories can bring almost 50% reduction of mass required on earth orbit under what suitable LH2/LO2 system provides; approach taken to study of escape stage booster performance; study results obtained.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Sizing nuclear orbital launch vehicles for interplanetary missions


    Weitere Titelangaben:

    Astronautics Aeronautics


    Beteiligte:

    Erschienen in:

    Erscheinungsdatum :

    1964


    Format / Umfang :

    7 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



    Orbital Magnetic Interplanetary Launch System (OMILS)

    Luis, Samuel / Khan, Mukit Azad | Springer Verlag | 2018


    Earth orbital operations supporting manned interplanetary missions

    Sherwood, Brent / Buddington, Patricia A. / Whittaker, William L. | NTRS | 1989


    Launch Windows for Orbital Missions

    A. H. Milstead | NTIS | 1964


    The indirect launch mode: a new launch technique for interplanetary missions

    Farquhar, R. W. / Dunham, D. W. / International Academy of Astronautics | British Library Conference Proceedings | 1999