Formulating an adequate statistical statement concerning space vehicle dynamic states requires the combination of the statistics of the environment and the vehicle's basic parameters. The basic ingredient of the environment for the Space Shuttle launch phase is the winds, which are represented by an ensemble of measured winds (150/month), which today constitute the best statistical representation. The problem treated in this paper then becomes twofold: (1) how can the vehicle response be analyzed using wind ensembles, and (2) how can the vehicle parameter variations be treated in conjunction with wind ensembles.


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    Titel :

    Computation of launch vehicle system requirements using hybrid computer.


    Beteiligte:
    Ryan, R. S. (Autor:in) / Ernsberger, G. R. (Autor:in) / Long, G. S. (Autor:in)

    Kongress:

    Summer Computer Simulation Conference ; 1973 ; Montreal, Canada


    Erscheinungsdatum :

    01.01.1973


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :



    Launch Vehicle Recovery System Requirements

    Barraza, R. M. | SAE Technical Papers | 1962


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