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367-80 airplane variable stability simulation system /NASA Langley supersonic transport simulation program/Four-engine jet aircraft used as in-flight simulator for variable stability testing of supersonic aircraft
Document ID
19660022563
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Person, S. D. (Boeing Co. Renton, WA, United States)
Robbins, R. E. (Boeing Co. Renton, WA, United States)
Date Acquired
August 3, 2013
Publication Date
January 1, 1965
Subject Category
Aircraft
Report/Patent Number
NASA-CR-66126
D6-19856
Report Number: NASA-CR-66126
Report Number: D6-19856
Accession Number
66N31853
Funding Number(s)
CONTRACT_GRANT: NAS1-4096
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
JET AIRCRAFT
STABILITY AND CONTROL
SUPERSONIC AIRCRAFT
FLIGHT SIMULATOR

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