Computer program has been developed as analytical tool to predict severity of effects of exhaust of rocket engines on adjacent spacecraft surfaces. Program computes forces, moments, pressures, and heating rates on surfaces immersed in or subjected to exhaust plume environments. Predictions will be useful in design of systems where such problems are anticipated.


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    Title :

    Study of high altitude plume impingement


    Contributors:

    Publication date :

    1972-10-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




    Study of high altitude plume impingement

    Mcanally, J. V. / Smith, S. D. | NTRS | 1973


    Study of High Altitude Plume Impingement

    J. V. Mcanally / S. D. Smith | NTIS | 1973


    Numerical modeling of transient plume impingement during high altitude rocket staging

    Eramya, A. / Cline, J. / Braunstein, M. et al. | British Library Conference Proceedings | 2007


    Numerical modeling of transient plume impingement during high altitude rocket staging

    Eramya, Allen / Cline, Jason / Braunstein, Matthew et al. | AIAA | 2007


    Space Shuttle Plume and Plume Impingement Study

    Tevepaugh, J. A. / Penny, M. M. | NTRS | 1977