Facility at Palo Alto research laboratories of Lockheed Missile Systems Div, designed to investigate problems associated with heating and stability during re-entry from ICBM trajectory or satellite orbit; Hot Shot Facility supplies power to "low speed" blowdown tunnel with Mach number range from 10 to 24, and high speed shock tube facility for range above 100; advantages of arc heated and shock tube wind tunnels, compared.


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    Titel :

    Lockheed arc-heated hypersonic tunnel


    Weitere Titelangaben:

    Soc Automotive Engrs -- Paper


    Beteiligte:
    Smelt, R. (Autor:in) / Turner, T.E. (Autor:in)

    Kongress:

    SAE Meeting ; 1958 Supersonic



    Erscheinungsdatum :

    1958


    Format / Umfang :

    19 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    LOCKHEED ARC-HEATED HYPERSONIC TUNNEL

    SMELT, RONALD / TURNER, T. E. | SAE Technical Papers | 1958


    Laser-heated hypersonic wind tunnel

    Buonadonna, V. / Knight, C. / Hertzberg, A. | Tema Archiv | 1973


    Laser-Heated Hypersonic Wind Tunnel

    VICTOR R. BUONADONNA / CHARLES J. KNIGHT AND A. HERTZBERG | AIAA | 1973


    Design Considerations for Arc Heated Hypersonic Tunnel

    P.M. SHERMAN / H.C. EARLY / W.N. LAWRENCE | NTIS | 1960


    Hypersonic, High-Density Stored Arc-Heated Air Wind Tunnel

    W.B. BOATRIGHT / A.P. SABOL / R.B. STEWART et al. | AIAA | 1972