Mach 6 experimental and theoretical stability and performance of a cruciform missile at angles of attack up to 65
By: Edward R. Hartman, Patrick J. Johnston.
Contributors: Johnston, Patrick J.; United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.
Series: NASA technical paper -- 2733.
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Office; For sale by the National Technical Information Service]
Published: 1987
Place of publication: [Washington, D.C.]; [Springfield, Va
Language: eng
Format: Microform
Subjects: Guided missiles -- Stability.
Other titles: Mach six experimental and theoretical stability and performance of a cruciform missile at angles of attack up to 65.
Notes: Distributed to depository libraries in microfiche.

Microfiche. [Washington, D.C.? : National Aeronautics and Space Administration], 1987. 1 microfiche.