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Free-flight Investigation of Longitudinal Stability and Control of a Rocket-propelled Missile Model Having Cruciform, Triangular, Inline Wings and Tails
Document ID
19930086932
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Hall, James R
Date Acquired
August 16, 2013
Publication Date
March 25, 1952
Report/Patent Number
NACA-RM-L51J17
Report Number: NACA-RM-L51J17
Accession Number
93R16222
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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