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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
19710065199
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Research Memorandum
Authors
Chubb, R. S. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 6, 2013
Publication Date
September 23, 1952
Subject Category
Unknown
Report/Patent Number
NACA-RM-A52G29
Report Number: NACA-RM-A52G29
Accession Number
71N70512
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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