Application of nonlinear aerodynamic stability characteristics to simplify missile control and guidance systems /
by Howard J. Curfman.

Description

Main Author

Curfman, Howard J.

Related Names

Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics.
United States. National Advisory Committee for Aeronautics.

Language(s)

English

Published

Washington, D.C. : National Advisory Committee for Aeronautics, 1955.

Subjects

Guided missiles > Guided missiles / Control systems > Guided missiles / Control systems / Aerodynamics.
Guidance systems (Flight) > Guidance systems (Flight) / Aerodynamics.

Note

"Declassified February 10, 1959."
"February 15, 1955."
Cover title.

Physical Description

23 p. : ill. ; 27 cm.

Locate a Print Version

Find in a library

Viewability