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Data requirements for in-flight synthesis and multiple blender studiesData requirements for in-flight synthesis and multiple blender studies to improve stability and control of large flexible boosters
Document ID
19660026359
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Edinger, L. D. (Honeywell, Inc. Saint Paul, MN, United States)
White, G. D. (Honeywell, Inc. Saint Paul, MN, United States)
Date Acquired
August 3, 2013
Publication Date
August 1, 1966
Subject Category
Electronics
Report/Patent Number
NASA-CR-548
Report Number: NASA-CR-548
Accession Number
66N35649
Funding Number(s)
CONTRACT_GRANT: NAS8-11206
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
FLEXIBLE BODY
STABILITY AND CONTROL
ENGINE CONTROL
CONTROL SYSTEM
FLIGHT CONTROL

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