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Manufacturing techniques for gyroscopes in gravity probe BThe design of the fused silica gyroscope configuration is presented. The first gyroscope was made for erection and spin tests only and does not contain the angle readout loops necessary for a functioning experimental gyroscope. The rotor ball described is not coated with the ultimate material, niobium, but instead with a sandwich of titanium, cooper, and titanium for spin-up test purposes. Background, historical information, manufacturing procedures, and sketches for this gyroscope are included to provide a better understanding of the device and the techniques and special tools required to manufacture a fused silica gyroscope to the required specifications.
Document ID
19760022465
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Rasquin, J. R.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 3, 2013
Publication Date
July 1, 1976
Subject Category
Instrumentation And Photography
Report/Patent Number
NASA-TM-X-73321
Report Number: NASA-TM-X-73321
Accession Number
76N29553
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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