Aerodynamic braking may be used as one means of slowing down vehicle preparatory to placing it into preassigned orbit about planet thus minimizing retrorocket requirements; this raises following problem -- what are steepest and shallowest angles at which spaceship may enter given atmosphere with given velocity; computational procedure is developed to determine thrust-augmented aerodynamic entry corridors and corresponding lift-to-drag programs and resultant trajectories; procedure is applied to study of thrust-augmented entry corridors for Mars for various vehicle characteristics and conditions.


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    Titel :

    Determination of extreme entry angles into planetary atmosphere


    Weitere Titelangaben:

    AIAA J


    Beteiligte:
    Warga, J. (Autor:in) / Hailey, W.C. (Autor:in)

    Erschienen in:

    AIAA Journal ; 2 , n 2


    Erscheinungsdatum :

    1964


    Format / Umfang :

    4 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :





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