Effect of longitudinal and lateral controls on winged reentry configuration at mach 1.97 and angles of attack up to 90° /
by Gerald V. Foster.

Description

Main Author

Foster, Gerald V.

Related Names

United States. National Aeronautics and Space Administration.

Language(s)

English

Published

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

Subjects

Angle of attack (Aerodynamics)
Space vehicles > Space vehicles / Atmospheric entry.

Note

"February 1961."

Physical Description

11 p. : ill. ; 26 cm.

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