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Flight measurements of stability and control derivatives of the x-15 research airplane to a mach number of 6.02 and an angle of attack of 25 degFlight test data on longitudinal, lateral, and directional stability and control derivatives of X-15 aircraft
Document ID
19650001037
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Yancey, R. B. (NASA Flight Research Center Edwards, CA, United States)
Date Acquired
September 2, 2013
Publication Date
November 1, 1964
Subject Category
Aircraft
Report/Patent Number
NASA-TN-D-2532
Report Number: NASA-TN-D-2532
Accession Number
65N10638
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
X-15 AIRCRAFT
STABILITY AND CONTROL
FLIGHT TEST

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