The report presents the results of a portion of a qualification overstress test on Hamilton Standard Rocket Engine Assembly 10-16, a nominal 0.2 footpounds thrust hydrazine monopropellant engine. This phase of the testing was concerned with verification of nozzle thrust coefficients and critical soakback testing of the REA.


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    Title :

    Overstress Qualification Test of the Multiple Satellite Dispenser 0.2 lbf Rocket Engine Assembly REA 10-16


    Contributors:

    Publication date :

    1973


    Size :

    41 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English