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Spacecraft boost and abort guidance and control systems requirement study, boost dynamics and control analysis study. Exhibit A: Boost dynamics and control anlaysisThe simulation developments for use in dynamics and control analysis during boost from liftoff to orbit insertion are reported. Also included are wind response studies of the NR-GD 161B/B9T delta wing booster/delta wing orbiter configuration, the MSC 036B/280 inch solid rocket motor configuration, the MSC 040A/L0X-propane liquid injection TVC configuration, the MSC 040C/dual solid rocket motor configuration, and the MSC 049/solid rocket motor configuration. All of the latest math models (rigid and flexible body) developed for the MSC/GD Space Shuttle Functional Simulator, are included.
Document ID
19730002163
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Williams, F. E.
(Boeing Co. Houston, TX, United States)
Price, J. B.
(Boeing Co. Houston, TX, United States)
Lemon, R. S.
(Boeing Co. Houston, TX, United States)
Date Acquired
September 2, 2013
Publication Date
September 15, 1972
Subject Category
Space Vehicles
Report/Patent Number
NASA-CR-128592
Report Number: NASA-CR-128592
Accession Number
73N10890
Funding Number(s)
CONTRACT_GRANT: NAS9-12183
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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