Aerodynamic damping and oscillatory stability in pitch and yaw of Gemini configurations at Mach numbers from 0.50 to 4.63 /
by Bruce R. Wright and Robert A. Kilgore.

Description

Main Author: Wright, Bruce R.
Related Names: Kilgore, Robert A.
Langley Research Center.
Language(s): English
Published: Washington, D.C. : National Aeronautics and Space Administration ; [1966]
Subjects: Project Gemini (U.S.)
Stability of space vehicles.
Space vehicles > Space vehicles / Atmospheric entry.
Yawing (Aerodynamics)
Pitching (Aerodynamics)
Vibration (Aeronautics) > Vibration (Aeronautics) / Damping.
Note: Errata sheet inserted.
Prepared at Langley Research Center.
"March 1966"--Cover.
Physical Description: 71 p. : ill. ; 27 cm.
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