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)


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    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




    Rocket thrust termination transients

    Rodean, H.C. | Engineering Index Backfile | 1959


    Hydroquench Thrust Termination Analysis

    D. P. Harry / N. S. Cohen | NTIS | 1973




    Injection thrust termination and modulation in solid rockets

    JAROUDI, R. / MCDONALD, A. J. | AIAA | 1964