Study shows weight comparison or trend data between different vehicles and heat protection schemes; application is to lifting and ballistic-type entry vehicles undertaking satellite and circumlunar missions; structural cooling methods examined include radiation, ablation, and combinations of these methods.


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    Titel :

    Parametric weight study of manned space entry vehicle


    Weitere Titelangaben:

    Aerospace Eng


    Beteiligte:

    Erschienen in:

    Aerospace Engineering ; 19 , n 10 ; p 40-49 + 77


    Erscheinungsdatum :

    1960


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Parametric study of manned aerocapture. II - Mars entry

    Lyne, J. E. / Anagnost, A. / Tauber, M. E. | NTRS | 1992


    Parametric study of manned aerocapture. II - Mars entry

    LYNE, J. E. / ANAGNOST, A. / TAUBER, M. E. | AIAA | 1992


    Manned Mars Entry Vehicle Aerothermodynamic Analysis

    Shizgal, Bernie D. / Weaver, David P. | AIAA | 1994


    Manned lifting entry.

    Love, E. S. | NTRS | 1966


    Manned lifting entry

    Love, E.S. | Engineering Index Backfile | 1966