Study of effects of aerodynamic derivatives and spin rate, re-entry angle and velocity, geostrophic winds, and drogue-parachute stabilizer on vehicle as it descended through atmosphere; considerable damping was necessary in low-speed portion of flight and damping could be enhanced by employing drogue parachute.


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    Title :

    Analytical investigation of dynamic behavior of nonlifting manned reentry vehicle


    Additional title:

    NASA -- Tech Note


    Contributors:


    Publication date :

    1960


    Size :

    55 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :