Simulation calculations of the Viking qualification flight tests are conducted by use of analytical models of the parachute deployment dynamics process. Results from the study indicate that good simulations of event times and trajectory are obtained. If the full-scale parachute drag coefficient is used, a good simulation of first opening load is obtained and the overall nature of the load history is calculated. For longitudinal motions, the two-degree-of-freedom models give good agreement with a six-degree-of-freedom model. It is believed that the analytical models used are tools which will aid in the analysis of future flight systems.


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    Titel :

    Postflight simulation of parachute deployment dynamics of Viking qualification flight tests


    Beteiligte:
    Whitlock, C. H. (Autor:in) / Poole, L. R. (Autor:in) / Talay, T. A. (Autor:in)

    Erscheinungsdatum :

    1973-09-01


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Postflight simulation of parachute deployment dynamics of Viking qualification flight tests

    Whitlock, Charles H. / Poole, Lamont R. / Talay, Theodore A. | TIBKAT | 1973


    The Viking parachute qualification test technique

    RAPER, J. / LUNDSTROM, R. / MICHEL, F. | AIAA | 1973


    The Viking parachute qualification test technique.

    Raper, J. L. / Lundstrom, R. R. / Michel, F. C. | NTRS | 1973