Wind-tunnel investigation at Mach numbers from 3.0 to 6.8 of the static aerodynamic characteristics of modified Mercury exit and escape capsule configurations /
by Albin O. Pearson.

Description

Main Author

Pearson, Albin O.

Related Names

Langley Research Center.
United States. National Aeronautics and Space Administration.

Language(s)

English

Published

Washington, [D.C.] : National Aeronautics and Space Administration, 1960.

Subjects

Mach number.
Stability of space vehicles.
Hypersonic wind tunnels.
Mercury probes.

Note

"September 1960."
Cover title.

Physical Description

19 p. : ill. ; 26 cm.

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