Entry corridor thermal entry limits for Apollo spacecraft defined for design of thermal protection system


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    Title :

    Definition of entry corridor thermal limits for Apollo spacecraft.


    Contributors:
    Curry, D. M. (author) / Posgay, R. G. (author) / Strouhal, G. (author)

    Conference:

    AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, ENTRY VEHICLE SYSTEMS AND TECHNOLOGY MEETING ; 1968 ; WILLIAMSBURG, VA


    Publication date :

    1968-12-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English


    Keywords :


    Definition of entry corridor thermal limits for Apollo spacecraft

    CURRY, D. / POSGAY, R. / STROUHAL, G. | AIAA | 1968




    Apollo spacecraft

    Osbon, H.G. | Engineering Index Backfile | 1964


    Apollo spacecraft.

    Low, G. M. | NTRS | 1969