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IUSThrust Vector Control (TVC) servo systemThe IUS TVC SERVO SYSTEM which consists of four electrically redundant electromechanical actuators, four potentiometer assemblies, and two controllers to provide movable nozzle control on both IUS solid rocket motors is developed. An overview of the more severe IUS TVC servo system design requirements, the system and component designs, and test data acquired on a preliminary development unit is presented. Attention is focused on the unique methods of sensing movable nozzle position and providing for redundant position locks.
Document ID
19790014390
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Conner, G. E.
(United Technologies Corp. East Hartford, CT, United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1979
Publication Information
Publication: NASA. Johnson Space Center The 13th Aerospace Mech. Symp.
Subject Category
Structural Mechanics
Accession Number
79N22561
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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