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Experimental Investigation of the Stability, Control, and Induced Rolling Moments of a Canard Missile Airframe at a Mach Number of 1.7
Document ID
19930087242
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Chubb, Robert S
Date Acquired
August 16, 2013
Publication Date
September 23, 1952
Report/Patent Number
NACA-RM-A52G29
Report Number: NACA-RM-A52G29
Accession Number
93R16532
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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