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Program documentation. Program description and user information for the hydraulics/auxiliary power unit (HYDRA) computer programA timeline containing altitude, control surface deflection rates and angles, hinge moment loads, thrust vector control gimbal rates, and main throttle settings is used to derive the model. The timeline is constructed from the output of one or more trajectory simulation programs.
Document ID
19790016501
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Redwine, W. J. (Lockheed Electronics Co. Houston, TX, United States)
Date Acquired
September 4, 2013
Publication Date
March 1, 1979
Subject Category
Computer Programming And Software
Report/Patent Number
LEC-13265
NASA-CR-160178
JSC-14805
Report Number: LEC-13265
Report Number: NASA-CR-160178
Report Number: JSC-14805
Accession Number
79N24672
Funding Number(s)
CONTRACT_GRANT: NAS9-15800
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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