A study to identify the optimum inclination for a satellite when the satellite is inclination non-sensitive and is to be retrieved is reported. This inclination is such that it provides an opportunity for a retrieval flight at least once each day with minimal on-orbit phasing requirements and minimal ascent performance losses. (Author)


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Optimum Inclination for Shuttle Retrieval of Inclination Non-Sensitive Satellites


    Beteiligte:

    Erscheinungsdatum :

    1973


    Format / Umfang :

    18 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





    Changing Inclination for Shuttle Payloads

    T.M. Spencer / R. Glickman / G. Porcellit | AIAA | 1979


    Efficient inclination control for geostationary satellites

    SLAVINSKAS, D. / BENDEN, W. | AIAA | 1985


    Efficient inclination control for geostationary satellites

    SLAVINSKAS, D. D. / DABBAGHI, H. / BENDEN, W. J. et al. | AIAA | 1988


    Low Inclination Circular Orbits for Remote Sensing Satellites

    Kamalaldin, K. / Okasha, M. | British Library Conference Proceedings | 2014