Aerodynamic characteristics of a Sparrow III missile model in the flow field of a generalized parent body at Mach 2.86 /
Robert L. Stallings Jr.

Description

Main Author: Stallings, Robert L.
Related Names: United States. National Aeronautics and Space Administration.
Language(s): English
Published: Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; 1981.
Subjects: Guided missiles.
Aerodynamics, Supersonic.
Note: "February 1984"--Cover.
Physical Description: 26 p. : ill. ; 28 cm.
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Item Link	Original Source
Full view	University of Illinois at Urbana-Champaign