Apollo afterbody heat transfer and pressure with and without ablation at Mach numbers 5.8 - 8.3


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    Title :

    Apollo afterbody heat transfer and pressure with and without ablation at M infinity of 5.8 to 8.3


    Contributors:
    Lee, G. (author) / Sundell, R. E. (author)

    Publication date :

    1966-09-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English