Wind-tunnel investigation at supersonic speeds of a remote-controlled canard missile with a free-rolling-tail brake torque system
By: A.B. Blair, Jr.
Contributors: United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Series: NASA technical paper -- 2401.
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Branch
Published: 1985
Place of publication: [Washington, DC]
Language: eng
Format: Microform
Subjects: Aerodynamics, Supersonic.
Other titles: Wind tunnel investigation at supersonic speeds of a remote controlled canard missile with a free rolling tail brake torque system.
Notes: Distributed to depository libraries in microfiche.

Microfiche. [Washington, D.C.? : National Aeronautics and Space Administration], 1987. 1 microfiche ; 11 x 15 cm.