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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