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Hydrostatic fluid bearing gyroThe design, fabrication, and testing are described of a thermal control assembly capable of precisely controlling the LDG-540 Gyro case temperature at 50 C over an ambient environment range of 23 C and atmosphere pressure to 5 C and a vacuum of 0.00001 torr. The thermal control assembly is a hermetically sealed enclosure about the LDG-540 Gyro with envelope dimensions not to exceed those of the Saturn K8-AB5 Gyro. The heaters are capable of delivery 30 watts at 28 V.D.C. and have dual temperature sensors rated at 750 ohms at 50 C. All six (6) LGD-540 Gyros will be equipped with a fine control heater and a resistance thermometer to monitor the gyro cast temperature. All six gyros will be interchangeable in the thermal control assembly by means of simply assembly techniques.
Document ID
19750015859
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Brello, E. Y.
(Bendix Corp. Teterboro, NJ, United States)
Date Acquired
September 3, 2013
Publication Date
March 1, 1975
Subject Category
Instrumentation And Photography
Report/Patent Number
NASA-CR-120753
Report Number: NASA-CR-120753
Accession Number
75N23931
Funding Number(s)
CONTRACT_GRANT: NAS8-24414
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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