Static longitudinal aerodynamic characteristics of several configurations used in the development of the Little Joe II-Apollo test vehicle at Mach numbers from 0.056 to 4.65 /
Robert H. Moore, Jr.

Description

Main Author

Moore, Robert H.

Related Names

Manned Spacecraft Center (U.S.)
United States. National Aeronautics and Space Administration.

Language(s)

English

Published

Washington, D.C. : National Aeronautics and Space Administration ; 1968.

Subjects

Launch vehicles (Astronautics) > Launch vehicles (Astronautics) / Longitudinal stability.
Space vehicles > Space vehicles / Aerodynamics > Space vehicles / Aerodynamics / Testing.

Note

Cover title.
"May 1968."

Physical Description

213 p. : ill. ; 26 cm.

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