Analysis of entry is developed around new dimensionless parameter which combines certain conditions at conic perigee altitude with certain characteristics of vehicle; parameter determines either deceleration- or heating-limited corridor widths for elliptic, parabolic, or hyperbolic approach trajectories; calculations of corridor widths and guidance problems presented for Venus, Earth, Mars, Jupiter, and Titan and curves for various entry conditions.


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    Titel :

    Analysis of corridor and guidance requirements for supercircular entry into planetary atmospheres


    Weitere Titelangaben:

    NASA -- Tech Report


    Beteiligte:
    Chapman, D.R. (Autor:in)


    Erscheinungsdatum :

    1959


    Format / Umfang :

    76 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :