The dynamic pressure time history after thrust termination is shown to be represented by a simple analytical approximation derived from powered flight trajectory parameters. The approximation is correlated with the results of accurate trajectory simulations. The agreement is adequate for 'ride-out' abort escape studies. (Author)


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    Titel :

    Dynamic Pressure Decay after Thrust Termination


    Beteiligte:
    P. W. Soule (Autor:in)

    Erscheinungsdatum :

    1965


    Format / Umfang :

    11 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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