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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    Title :

    Review of development of high enthalpy aerodynamic test facilities


    Additional title:

    Applied Mechanics Rev


    Contributors:

    Published in:

    Publication date :

    1960


    Size :

    4 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :