Static longitudinal stability characteristics of various Mercury escape configurations and of a proposed alternate escape configuration for Mach numbers of 0.05 to 9.60 /
by Robert P. Smith and William C. Moseley, Jr.
|Main Author:||Smith, Robert P.|
|Related Names:||Moseley, William C.|
Washington, D.C. : National Aeronautics and Space Administration, 1961.
Fighter planes /
Fighter planes / Safety measures /
Jet fighter planes > Jet fighter planes / Wind tunnel testing.
Aerodynamics > Aerodynamics / Testing.
Angle of attack (Aerodynamics) > Angle of attack (Aerodynamics) / Testing.
Stability of airplanes, Longitudinal > Stability of airplanes, Longitudinal / Testing.
Survival and emergency equipment > Survival and emergency equipment / Testing.
Full text also available online. Address as of 11/12/2010:
180 p. :
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