Attempt made to define maximum re-entry performance required of lifting re-entry vehicle, within limits imposed by maximum re-entry velocity of 36,000 fps; corresponding thermal environments established provide basis for examination of various thermal protection system concepts; systems which are believed sufficiently promising to justify further development are shown.


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    Titel :

    Thermal protection of lifting re-entry vehicles


    Weitere Titelangaben:

    Aerospace Eng


    Beteiligte:
    Dukes, W.H. (Autor:in) / Anthony, F.M. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1963


    Format / Umfang :

    17 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



    Flowfield predictions about lifting entry vehicles

    NICOLET, W. / SHANKS, S. / SRINIVASAN, G. et al. | AIAA | 1982


    Drive for lifting re-entry vehicles

    Fredette, R.E. / Orazio, F.D. | Engineering Index Backfile | 1961


    Thermal protection of ballistic entry vehicles

    REINIKKA, E. A. / SARTELL, R. J. | AIAA | 1965


    Charring ablators on lifting entry vehicles

    REINIKKA, E. A. / WELLS, P. B. | AIAA | 1964