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A Theoretical Investigation of the Effect of a Target Seeker Sensitive to Pitch Attitude on the Dynamic Stability and Response Characteristics of a Supersonic Canard Missile Configuration
Document ID
19930087147
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Gates, Ordway B , Jr
Schy, Albert A
Date Acquired
August 16, 2013
Publication Date
August 26, 1952
Report/Patent Number
NACA-RM-L52E19
Report Number: NACA-RM-L52E19
Accession Number
93R16437
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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