Design requirements show that for most altitude tests of rocket engines pressure altitude of 200,000 ft or less will meet major test objectives; however, jet impingment and jet spreading experiments require altitudes in excess of this value; development tests conducted at Arnold Center in support of Titan ICBM and Minuteman; requirements for exhaust gas handling system, including pumping and cooling requirements, are examined as function of engine size; characteristics of required test cells; installation and instrumentation support equipment.


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    Titel :

    High-altitude tests of rocket engines in ground test facilities


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:

    Kongress:

    SAE Meeting ; 1964 Testing



    Erscheinungsdatum :

    1964


    Format / Umfang :

    17 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    High-Altitude Tests of Rocket Engines in Ground Test Facilities

    Ferrell, Joel / Smith, Robert E. | SAE Technical Papers | 1964


    Rocket altitude test facilities register

    Ducasse, P. | TIBKAT | 1987



    Altitude Simulation Facilities For Rocket Test Firing

    Westcot, G. D. / Hausman, J. E. | SAE Technical Papers | 1964


    Altitude simulation facilities for rocket test firing

    Westcot, G.D. / Hausman, J.E. | Engineering Index Backfile | 1964