An advanced two-body six-degree-of-freedom computer model employing an indeterminate structures approach has been developed for the parachute deployment process. The program determines both vehicular and decelerator responses to aerodynamic and physical property inputs. A better insight into the dynamic processes that occur during parachute deployment has been developed. The model is of value in sensitivity studies to isolate important parameters that affect the vehicular response.


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    Titel :

    An advanced technique for the prediction of decelerator system dynamics.


    Beteiligte:
    Talay, T. A. (Autor:in) / Morris, W. D. (Autor:in) / Whitlock, C. H. (Autor:in)

    Kongress:

    Aerodynamic Deceleration Systems Conference ; 1973 ; Palm Springs, CA


    Erscheinungsdatum :

    01.05.1973


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    An Advanced Technique for the Prediction of Decelerator System Dynamics

    THEODORE A. TALAY / W. DOUGLAS MORRIS / AND CHARLES H. WHITLOCK | AIAA | 1973


    An advanced technique for the prediction of decelerator system dynamics

    TALAY, T. / MORRIS, W. / WHITLOCK, C. | AIAA | 1973


    Low Density Supersonic Decelerator Parachute Decelerator System

    Gallon, John C. / Clark, Ian G. / Rivellini, Tommaso P. et al. | NTRS | 2013


    Low Density Supersonic Decelerator Parachute Decelerator System

    Gallon, John / Witkowski, Allen / Clark, Ian G. et al. | AIAA | 2013


    Low Density Supersonic Decelerator Parachute Decelerator System

    Gallon, J. / Witkowski, A. / Clark, I.G. et al. | British Library Conference Proceedings | 2013