Tests were conducted on a rocket exhaust scavenging system as part of a program to develop new techniques for testing at simulated space conditions. Detailed plume characteristics were computed, and a model scavenging system was tested for both cold and hot gas rockets. Results indicate that for the firing of a typical small control rocket it will be possible to maintain 0.0001 torr pressure in a space chamber. (Author)


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    Titel :

    Investigation of Scavenging Systems for Removal of Rocket Exhaust Gases from Space Simulation Chambers


    Beteiligte:
    J. A. Morris (Autor:in) / D. E. Anderson (Autor:in)

    Erscheinungsdatum :

    1966


    Format / Umfang :

    2 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch