Summary of requirements to consider in study of return, re-entry and recovery; reference made to Douglas thick-wing planetary vehicle which provides means of reducing maximum heating rate and total heating by entering atmosphere with winged vehicle placed at high total angle of attack; re-entry fundamentals; balloons and gliders; other concepts such as use of magnetohydrodynamic principles for increasing re-entry drag.


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    Titel :

    To hit entry corridor -- Descending space vehicles should have variable drag


    Weitere Titelangaben:

    Missiles Rockets


    Beteiligte:
    Herrick, J.W. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1961


    Format / Umfang :

    2 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


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