The parameter defining the Keplerian phase of the reentry mission of a winged vehicle descending from circular low Earth orbit into atmosphere at 120 km altitude was studied. Entry parameter variations with deorbiting maneuver characteristics, and their sensitivities were analyzed.


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    Titel :

    Study on Reentry Guidance and Control. Volume 3: Reentry Trajectory Simulation


    Beteiligte:
    H. Grallert (Autor:in)

    Erscheinungsdatum :

    1988


    Format / Umfang :

    502 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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