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Flight Investigation at Supersonic Mach Numbers of an Automatic Acceleration Control Missile in which Rate Damping Is Obtained from a Linear Accelerometer Placed Ahead of the Missile Center of Gravity
Document ID
19930088908
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Seaberg, Ernest C
Sproull, Royce H
Reid, H J E , Jr
Date Acquired
August 16, 2013
Publication Date
November 8, 1955
Report/Patent Number
NACA-RM-L55G29
Report Number: NACA-RM-L55G29
Accession Number
93R18198
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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