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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    Title :

    Dynamic Pressure Decay after Thrust Termination


    Contributors:
    P. W. Soule (author)

    Publication date :

    1965


    Size :

    11 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English