Studies carried out by U S Air Force Aero Propulsion Laboratory on effects of subsonic flight environment on fuels refined for high Mach number application; high temperature fuel property requirements and hydrocarbon composition to meet these requirements; fuel compositions and low temperatures; results of wing tank pumpability tests; materials compatibility of high temperature fuels; it is concluded that establishment of specification criteria to obtain high temperature fuel suitable for subsonic and supersonic use will adversely affect cost and availability of product.


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    Titel :

    High temperature hydrocarbon fuels and subsonic flight environments


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Hager, J.A. (Autor:in)

    Kongress:

    SAE Meeting ; 1965



    Erscheinungsdatum :

    1965


    Format / Umfang :

    10 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



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