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Theoretical Investigation of the Stability at Negative Static Margins of a Supersonic Missile With an Autopilot Sensitive to Pitch Angle and Pitching Velocity
Author:
Cole, Henry A., Jr.
Year:
1952
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-A52A14
Link:
https://digital.library.unt.edu/ark:/67531/metadc59176/
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