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The Longitudinal Stability and Control Characteristics of a 60 Degree Delta-wing Missile Having Half-delta Tip Controls as Obtained from a Free-flight Investigation at Transonic and Supersonic Speeds
Document ID
19930087329
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Moul, Martin T
Baber, Hal T , Jr
Date Acquired
August 16, 2013
Publication Date
October 3, 1952
Report/Patent Number
NACA-RM-L52H14
Accession Number
93R16619
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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