A preliminary investigation of modified blunt 13° half-cone re-entry configurations at subsonic speeds / George C. Kenyon and George G. Edwards.
|Main Author:||Kenyon, George C.|
|Other Authors:||Edwards, George G.|
Washington, D.C. : National Aeronautics and Space Administration, 1961.
Supersonic wind tunnels.
Wind tunnel testing.
Cone > Aerodynamics.
Space vehicles > Landing.
Space vehicles > Atmospheric entry.
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48 p. :
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