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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
Document ID
19930087033
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Cole, Henry, A , jr
Abramovitz, Marvin
Date Acquired
August 16, 2013
Publication Date
March 17, 1952
Report/Patent Number
NACA-RM-A52A14
Report Number: NACA-RM-A52A14
Accession Number
93R16323
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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