Computer program calculates forces, heating, and contamination. Source Flow Impingement Program (SFPLIMP), a computer program that analyzes impingement of exhaust from several rocket engines on nearby surfaces in vacuum. Designed to calculate quickly undesired forces, heating, and contamination caused by firing attitude-control jets toward other surfaces of controlled spacecraft.


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    Titel :

    Impingement Of Rocket Exhaust


    Beteiligte:

    Erschienen in:

    Erscheinungsdatum :

    1988-04-01



    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Rocket exhaust impingement on ground surface

    Yoshihara, H. | Engineering Index Backfile | 1963


    Material evaluation under direct rocket exhaust impingement

    FREDERICKS, J. / SHORR, M. | AIAA | 1972


    Material Evaluation under Direct Rocket Exhaust Impingement

    J. T. FREDERICKS AND M. SHORR Bell Aerospace Division of Textron / Buffalo / N. Y. | AIAA | 1973



    Rocket-exhaust impingement on a flat plate at high vacuum.

    KOPPANG, R. R. / PIESIK, E. T. | AIAA | 1966