Hypersonic flight vehicle

B - Operations – Transporting – 64 – D

Patent

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Details

244/13, 60/63

B64D 27/10 (2006.01) F02C 7/04 (2006.01)

Patent

CA 2010385

ABSTRACT OF THE DISCLOSURE A hypersonic inlet and a hypersonic engine and flight vehicle having such an inlet. The three-dimensionally-swept inlet has an upper member with a caret-shaped lower surface portion producing a two-dimensional wedge flow below such lower surface portion. The inlet also has a lower member having two inverted and transposed semi-caret-shaped upper surface portions producing a two-dimensional wedge flow above such upper surface portions. An inlet aft portion connects together the upper and lower members and has an orifice defining the engine inlet throat which at least partially receives the two-dimensional flows. 17

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