Wind-tunnel investigation at supersonic speeds of a remote-controlled canard missile with a free-rolling-tail brake torque system [microform] / A.B. Blair, Jr.
Published
[Washington, DC] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.
Physical Description
1 v.
Notes
Distributed to depository libraries in microfiche.
Microfiche. [Washington, D.C.? : National Aeronautics and Space Administration], 1987. 1 microfiche ; 11 x 15 cm.
Variant and related titles
Wind tunnel investigation at supersonic speeds of a remote controlled canard missile with a free rolling tail brake torque system.