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Summary of preliminary data derived from the XB-70 airplanesPreliminary data of handling, thermal response, propulsion system, noise, and sonic boom for XB-70
Document ID
19660018723
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Andrews, W. H. (NASA Flight Research Center Edwards, CA, United States)
Date Acquired
September 2, 2013
Publication Date
June 1, 1966
Subject Category
Aircraft
Report/Patent Number
NASA-TM-X-1240
Accession Number
66N28013
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
PERFORMANCE CHARACTERISTICS
SUPERSONIC TRANSPORT
FLIGHT TEST

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