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On-orbit checkout studyThe spaceborne testing equipment carried by the orbiter and the measuring equipment onboard the satellite (telemetry) is tested to verify that each is operating satisfactorily. The satellite command system is also checked. Thermal stabilization with the satellite in the orbiter shadow is achieved in six to eight hours. Satellite subsystem tests are run, and thermal control by heaters is checked. Thermal stabilization with the satellite exposed to the sun (when the orbiter is in sunlight) is again achieved in an estimated six to eight hours. Subsystem tests are again run in the hot condition, and heat rejection tests are made.
Document ID
19770015219
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Pritchard, E. I.
(Aerospace Corp. El Segundo, CA, United States)
Date Acquired
September 3, 2013
Publication Date
January 13, 1977
Subject Category
Space Transportation
Report/Patent Number
NASA-CR-152682
ATR-76(7372-01)-1
Report Number: NASA-CR-152682
Report Number: ATR-76(7372-01)-1
Accession Number
77N22163
Funding Number(s)
CONTRACT_GRANT: NASW-2884
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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