Stability and control characteristics at Mach numbers from 0.20 to 4.63 of a cruciform air-to-air missile with triangular canard controls and a trapezoidal wing /
by Ernald B. Graves and Roger H. Fournier.

Description

Main Author

Graves, Ernald B.

Related Names

Fournier, Roger H.
Langley Research Center.

Language(s)

English

Published

Washington, D.C. : National Aeronautics and Space Administration ; 1974.

Subjects

Guided missiles > Guided missiles / Aerodynamics > Guided missiles / Aerodynamics / Statistics.
Guided missiles > Guided missiles / Control systems > Guided missiles / Control systems / Statistics.
Guided missiles > Guided missiles / Stability > Guided missiles / Stability / Statistics.

Note

Prepared at Langley Research Center.
Errata sheet inserted.
Chiefly graphs.
Cover title.

Physical Description

233 p. : ill. ; 27 cm.

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