High Altitude Decelerator Systems are used to provide a stable descending platform when deployed from a sounding rocket at altitudes greater than 40 kilometers allowing a scientific mission to be conducted in a specific altitude region. The High Altitude Decelerator is designed to provide a highly stable, high drag area system packed in a minimum volume to deploy successfully from a sounding rocket. Deployment altitudes greater than 100 kilometers have been successfully demonstrated at dynamic pressures as low as 0.004 pounds per square foot.


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    Titel :

    High altitude decelerator systems


    Beteiligte:

    Kongress:

    AIAA Aerodynamic Decelerator Systems Technology Conference ; 1989 ; Cocoa Beach, FL, United States


    Erscheinungsdatum :

    01.01.1989


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    High altitude decelerator systems

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


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