The report presents the results of a portion of a Qualification Overstress Test on Hamilton Standard Rocket Engine Assembly, Model 16-10, a nominal 0.2 pound thrust monopropellant engine. The purpose of the tests performed was to establish engine characteristics over extended life and to establish performance parameters over a range of operating conditions.


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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 :

    197 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English