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.
Review of development of high enthalpy aerodynamic test facilities
Applied Mechanics Rev
Applied Mechanics Reviews ; 13 , n 6
1960
4 pages
Article (Journal)
English
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Test Facilities for High Enthalpy Planetary Entry Simulation
British Library Conference Proceedings | 2006
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