The report describes a system that was developed for use in a test in which the thermally stressed nozzle of a liquid rocket engine would be exposed to nuclear readiation. To accomplish this objective the system developed had to be capable of firing the engine at a simulated 100,000 foot altitude and exposing the chamber throat immediately after firing to a nuclear beam.


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    Titel :

    Development of a System for Exposing a Thermally Stressed Liquid Rocket Nozzle to Nuclear Radiation


    Beteiligte:
    J. E. Hewes (Autor:in)

    Erscheinungsdatum :

    1973


    Format / Umfang :

    31 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch