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Inertial reference unitUnit provides rate damping, linear velocity changes and angular position information to attitude control system during turns and motor burns.
Document ID
19720000094
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Crawford, R. A.
Date Acquired
August 6, 2013
Publication Date
January 1, 1972
Subject Category
Electronic Systems
Report/Patent Number
NPO-11518
Report Number: NPO-11518
Accession Number
72B10094
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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