Objective of hypersonic propulsion research and design of Hypersonic Propulsion Laboratory at Applied Physics Laboratory of John Hopkins University for inlet and combustion testing of air-breathing engines; program resulted in arc tunnel operation at pressures up to 800 psi, with running times up to 2-min and power inputs (single unit) up to 8.6 Mw; description of h-p arc heaters, power supply, and operating principles and electrode design; performance of arc unit and constructions of Mach 7-10 propulsion tunnel with emphasis on nozzle geometry.


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    Titel :

    Development of hypersonic propulsion tunnels using D.C. Plasma arc heating


    Weitere Titelangaben:

    AIAA-ASME -- Paper


    Beteiligte:
    Raezer, S.D. (Autor:in) / Bunt, E.A. (Autor:in) / Olsen, H.L. (Autor:in)

    Kongress:

    AIAA-ASME Hypersonic Ramjet Conference ; 1963 Supersonic


    Erschienen in:

    Erscheinungsdatum :

    1963


    Format / Umfang :

    13 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



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    Application of d.c. plasma arc heating to hypersonic propulsion testing

    BUNT, E. A. / OLSEN, H. L. / RAEZER, S. D. | AIAA | 1964