Propulsion Engine Test Cell at Rocket Test Facility, Arnold Center is described; discussion is concerned with tests of 16,000-lb-thrust engine, which was fired with combustion products removed by plant exhausters, and full-scale reaction control system rocket, which was fired with combustion products removed by chamber pumping systems only; chamber performance and operating experience are presented with respect to these tests; test firings of full-scale rocket engines at starting pressure altitudes above 350,000 ft in J-2A chamber demonstrated feasibility of space-system propulsion testing at near-space pressure and temperature conditions.


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    Titel :

    Performance and operating experience of space simulation chamber used for propulsion testing


    Weitere Titelangaben:

    J Environmental Sciences


    Beteiligte:

    Erschienen in:

    Erscheinungsdatum :

    1965


    Format / Umfang :

    7 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :