Basic design requirements; spectrum of all possible hypersonic vehicles may be divided into regions characterized by Mach numbers from 5 to 10 which fly continuously in so-called "Flight Corridor", and those vehicles characterized by Mach numbers of 20 which operate at or near orbital speeds and are capable of leaving and subsequently re-entering atmosphere via flight corridor; spaceheater facilities for testing such vehicles is described.


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    Titel :

    Review of development of high enthalpy aerodynamic test facilities


    Weitere Titelangaben:

    Applied Mechanics Rev


    Beteiligte:
    Henshall, B.D. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1960


    Format / Umfang :

    4 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :