A parametric pretest uncertainty analysis has been performed for a chemical rocket engine test at a unique 1000:1 area ratio altitude test facility. Results from the parametric study provide the error limits required in order to maintain a maximum uncertainty of 1 percent on specific impulse. Equations used in the uncertainty analysis are presented.


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    Title :

    Pretest Uncertainty Analysis for Chemical Rocket Engine Tests


    Contributors:

    Publication date :

    1987


    Size :

    16 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





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