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.

Description

Main Author

Smith, Robert P.

Related Names

Moseley, William C.
United States. National Aeronautics and Space Administration.

Language(s)

English

Published

Washington, D.C. : National Aeronautics and Space Administration, 1961.

Subjects

Fighter planes > Fighter planes / Safety measures > Fighter planes / Safety measures / Testing.
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.

Note

"July 1961."
Cover title.
Full text also available online. Address as of 11/12/2010:

Physical Description

180 p. : ill. ; 26 cm.

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