Prediction of flight performance has been dependent upon sea-level data that must be extrapolated to flight configuration; errors up to 4% in predicted specific impulse resulted because of inability to identify factors affecting extrapolation; technique permits estimation of specific impulse within 2% for conventional propellant systems at any exit area ratio with no test data; if sea-level test data are available, altitude performance can be estimated within 1%; effects of mixture ratio-distribution and interactions between injector chamber performance and nozzle are responsible for most of errors using characteristic velocity-thrust coefficient method.


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    Titel :

    Improved method for rocket performance prediction


    Weitere Titelangaben:

    J Spacecraft Rockets


    Beteiligte:
    Valentine, R.S. (Autor:in) / Dean, L.E. (Autor:in) / Pieper, J.L. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1966


    Format / Umfang :

    6 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    An improved method for rocket performance prediction.

    DEAN, L. E. / PIEPER, J. L. | AIAA | 1966


    Rocket Performance Prediction Technique

    J. H. Morgenthaler / W. R. Stepien | AIAA | 1975


    Hybrid Rocket Propulsion Performance Prediction

    Cavalleri, R. J. / Loehr, R. D. / American Institute of Aeronautics and Astronautics et al. | British Library Conference Proceedings | 2005


    Solid rocket performance prediction techniques

    COHEN, N. / HARRY, III, D. / PRICE, C. et al. | AIAA | 1974


    Hybrid Rocket Propulsion Performance Prediction

    Cavalleri, Robert / Loehr, Richard | AIAA | 2005