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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    Title :

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


    Contributors:
    H. Grallert (author)

    Publication date :

    1988


    Size :

    502 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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