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Development of control systems for space shuttle vehicles. Volume 2: AppendixesA launch phase random normal wind model is presented for delta wing, two-stage, space shuttle control system studies. Equations, data, and simulations for conventional launch studies are given as well as pitch and lateral equations and data for covariance analyses of the launch phase of MSFC vehicle B. Lateral equations and data for North American 130G and 134D are also included along with a high-altitude abort simulation.
Document ID
19720003293
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Stone, C. R. (Honeywell, Inc. Minneapolis, MN, United States)
Chase, T. W. (Honeywell, Inc. Minneapolis, MN, United States)
Kiziloz, B. M. (Honeywell, Inc. Minneapolis, MN, United States)
Ward, M. D. (Honeywell, Inc. Minneapolis, MN, United States)
Date Acquired
September 2, 2013
Publication Date
September 1, 1971
Publication Information
Publisher: NASA
Subject Category
Space Vehicles
Report/Patent Number
NASA-CR-1900
HONEYWELL-14257-FR-VOL-2
Accession Number
72N10942
Funding Number(s)
CONTRACT_GRANT: NAS8-25181
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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