The heavyweight motor development, the lightweight motor design and the propellant re-evaluation were completed. The final heavyweight motor test results are presented along with the data plots and photographs. The motor was fired at simulated altitude and successfully extinguished.


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    Titel :

    Feasibility Demonstration of a Single-Chamber Controllable Solid Rocket Motor


    Beteiligte:
    C. T. Levinsky (Autor:in) / G. F. Kobalter (Autor:in)

    Erscheinungsdatum :

    1966


    Format / Umfang :

    106 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch