Geostationary transfer orbit (GTO) characteristics of former geosynchronous satellites; satellite configurations as to GTO requirements; telemetry and telecommand, thermal, power, and attitude control subsystems as to stabilization modes and GTO constraints; and apogee injection strategies (single/multiple burn, steering law) were reviewed. The investigations were confined to 2 Ariane 4 payload classes (2500 kg in GTO, dual-launch and 4200 kg in GTO, single launch), three-axis or slow barbecue stabilization during transfer orbit, and use of a liquid apogee injection system with low thrust level (400 N). A recommendation for an overall system optimization is presented.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Study of the Optimization of Satellite System Design for Transfer Orbit


    Beteiligte:
    by Baet (Autor:in) / K. Fetzer (Autor:in) / W. Fink (Autor:in) / H. Hufnagel (Autor:in) / H. Kellermeier (Autor:in)

    Erscheinungsdatum :

    1983


    Format / Umfang :

    349 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





    Orbit transfer strategy optimization method for orbit injection of large elliptical frozen orbit satellite

    LI JIAN / CHEN XIANG / XIA YONG et al. | Europäisches Patentamt | 2023

    Freier Zugriff

    Multidisciplinary system design optimization of on orbit satellite assembly architectures

    Sternberg, David / Chodas, Mark / Jewison, Chris et al. | IEEE | 2015


    SATELLITE TRANSFER ORBIT SEARCH METHODS

    MCNAIR STEPHANIE LAUREN / BYSTROFF JOHN ROMAN / POOL CALEB LUKE | Europäisches Patentamt | 2017

    Freier Zugriff

    SATELLITE TRANSFER ORBIT SEARCH METHODS

    STEPHANIE LAUREN MCNAIR / JOHN ROMAN BYSTROFF / CALEB LUKE POOL | Europäisches Patentamt | 2016

    Freier Zugriff