Parachute design for decelerating upper atmosphere rocket probes at high altitudes, using high drag coefficients in Stokes flow regime


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    Title :

    Development of an extremely lightweight, high- altitude decelerator


    Contributors:

    Conference:

    AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, AERODYNAMIC DECELERATION SYSTEMS CONFERENCE, 2ND ; 1968 ; EL CENTRO, CA


    Publication date :

    1969-11-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English


    Keywords :




    High altitude decelerator systems

    Silbert, Mendel N. / Moltedo, A. David / Gilbertson, Gaylord S. | NTRS | 1989



    High altitude decelerator systems

    SILBERT, MENDEL / MOLTEDO, A. / GILBERTSON, GAYLORD | AIAA | 1989