Longitudinal stability and control characteristics from a flight investigation of a cruciform canard missile configuration having an exposed wing-canard area ratio of 16:1 /
by Martin T. Moul and Andrew R. Wineman.

Description

Main Author

Moul, Martin T.

Related Names

Wineman, Andrew R.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics.

Language(s)

English

Published

Washington, D.C. : National Advisory Committee for Aeronautics, 1952.

Subjects

Stability of airplanes, Longitudinal.
Rockets (Aeronautics) > Rockets (Aeronautics) / Canard fins.

Note

"June 25, 1952."

Physical Description

33 p. : ill. ; 27 cm.

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