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Use of computer modeling to investigate a dynamic interaction problem in the Skylab TACS quad-valve packageA valve opening-response problem encountered during development of a control valve for the Skylab thruster attitude control system (TACS) is described. The problem involved effects of dynamic interaction among valves in the quad-redundant valve package. Also described is a detailed computer simulation of the quad-valve package which was helpful in resolving the problem.
Document ID
19760012101
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hesser, R. J. (McDonnell-Douglas Astronautics Co. Huntington Beach, CA, United States)
Gershman, R. (McDonnell-Douglas Astronautics Co. Huntington Beach, CA, United States)
Date Acquired
August 8, 2013
Publication Date
August 1, 1975
Publication Information
Publication: NASA. Kennedy Space Center 9th Aerospace Mech. Symp.
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
76N19189
Funding Number(s)
CONTRACT_GRANT: NAS9-6555
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19760012084Collected WorksThe 9th Aerospace Mechanisms Symposium
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