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Large space telescope control moment gyro test programThe underlying theory and design of test instrumentation and computer techniques used to determine the power spectral density (PSD) of the third generation gyro are described in detail. Acceptance test results on the completed instrument are presented as well as composite PSD plots. The measured RMS noise over the frequency band 0.0025 - 10 Hz was 0.012 arc seconds. Results obtained at Martin Company indicate an RMS noise of 0.009 arc seconds (0.05 - 10 Hz). The results obtained showed the TGG performance was close to the proposed LST requirements but that additional development work would be needed to reduce the TGG noise to within more desirable limits.
Document ID
19750025298
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Salamin, E.
(Draper (Charles Stark) Lab., Inc. Cambridge, MA, United States)
Bukow, G. J.
(Draper (Charles Stark) Lab., Inc. Cambridge, MA, United States)
Date Acquired
September 3, 2013
Publication Date
July 1, 1975
Subject Category
Instrumentation And Photography
Report/Patent Number
NASA-CR-143973
R-896
Report Number: NASA-CR-143973
Report Number: R-896
Accession Number
75N33371
Funding Number(s)
CONTRACT_GRANT: NAS8-30249
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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