Investigation of the Static Stability Characteristics of a Reentry Spacecraft Model in Free Flight for Mach Numbers from 2.62 to 1.11 Launched at an Angle of Attack of 180°

Investigation of the Static Stability Characteristics of a Reentry Spacecraft Model in Free Flight for Mach Numbers from 2.62 to 1.11 Launched at an Angle of Attack of 180°
Author: J. W. Usry
Publisher:
Total Pages: 32
Release: 1961
Genre: Angle of attack (Aerodynamics)
ISBN:

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