Atmosphere entry at parabolic speed with hypersonic glider provides for glide, within atmosphere to preselected landing site; phases considered are: entry maneuvers involving pull-out from initial dive into atmosphere and pull-up to suitable glide altitude just above satellite speed; global range control during transsatellite glide; and sub-satellite banked glide to recovery site with lateral offset control and minor range control maneuvers.


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    Title :

    Supercircular entry and recovery with maneuverable manned vehicles


    Additional title:

    Aerospace Eng


    Contributors:
    Smith, R.H. (author) / Menard, J.A. (author)

    Published in:

    Publication date :

    1961


    Size :

    7 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    Manned maneuverable reentry

    Stambler, I. | Engineering Index Backfile | 1964


    Entry monitor system for maneuverable vehicles

    Frank, A.J. / Knotts, E.F. / Johnson, B.C. | Engineering Index Backfile | 1966


    An entry monitor system for maneuverable vehicles.

    FRANK, A. J. / JOHNSON, B. C. | AIAA | 1966


    An entry monitor system for maneuverable vehicles

    FRANK, A. / JOHNSON, B. | AIAA | 1965


    An entry monitor system for maneuverable vehicles.

    Frank, A. J. / Johnson, B. C. / Knotts, E. F. | NTRS | 1966