The report presents the results of a portion of a Qualification Overstress Test on Hamilton Standard Rocket Engine Assembly, Model 16-9, a nominal 5.0 pound thrust monopropellant engine. The objectives of this portion of the Qualification Overstress Tests were to characterize the engine over extended life and at various operating conditions.


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    Title :

    Overstress Qualification Test of the Multiple Satellite Dispenser 5 LBF Rocket Engine Assembly REA 16-9


    Contributors:
    J. Genovese (author)

    Publication date :

    1973


    Size :

    196 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English