Two design options were explored to address the requirement to provide lunar piloted missions with continuous communications for outpost and sortie missions. Two unique orbits were assessed, along with the appropriate spacecraft (S/C) to address these requirements. Both constellations (with only two S/C each) provide full time coverage (24 hr/7 d) for a south polar base and also provide continuous 7 day coverage for sorties for specified sites and periodic windows. Thus a two-satellite system can provide full coverage for sorties for selected windows of opportunity without reconfiguring the constellation.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    COMPASS Final Report: Lunar Network Satellite-High Rate (LNS-HR)


    Beteiligte:
    S. R. Oleson (Autor:in) / M. L. McGuire (Autor:in)

    Erscheinungsdatum :

    2012


    Format / Umfang :

    114 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    COMPASS Final Report: Lunar Network Satellite-High Rate (LNS-HR)

    oleson, Steven R. / McGuire, Melissa L. | NTRS | 2012


    COMPASS Final Report: Lunar Relay Satellite (LRS)

    S. R. Oleson / M. L. McGuire | NTIS | 2012


    COMPASS Final Report: Lunar Relay Satellite (LRS)

    Oleson, Steven R. / McGuire, Melissa L. | NTRS | 2012


    COMPASS Final Report: Low Cost Robotic Lunar Lander

    M. L. McGuire / S. R. Oleson | NTIS | 2010


    COMPASS Final Report: Low Cost Robotic Lunar Lander

    McGuire, Melissa L. / Oleson, Steven R. | NTRS | 2010