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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    Titel :

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


    Beteiligte:

    Erscheinungsdatum :

    1973


    Format / Umfang :

    197 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch