Spacecraft deceleration upon entry into Mars orbit by aerodynamic braking, considering vehicle shape and velocity effects on entry heating


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    Title :

    Spacecraft heat-protection requirements for mars aerodynamic braking.


    Contributors:
    Hanley, G. M. (author) / Lyon, F. J. (author)

    Publication date :

    1965-08-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English