Aerodynamic characteristics of a Sparrow III missile model in the flow field of a generalized parent body at Mach 2.86
By: Robert L. Stallings Jr
Contributors: United States. National Aeronautics and Space Administration. Scientific and Technical Information Office
Series: NASA technical memorandum -- 85713
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Office; For sale by the National Technical Information Service]
Published: 1984
Place of publication: Washington, D.C; [Springfield, Va
Language: eng
Number of pages: 26
Subjects: Aerodynamics, Supersonic; Guided missiles
Notes: "February 1984"--Cover

Includes bibliographical references