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Assessment of Atomic Oxygen Erosion of Silver Interconnects on Intelsat 6, F3Intelsat 6 F-3 was launched from Cape Canaveral on a Titan 3 launch vehicle. Failure of the launch vehicle resulted in the satellite being marooned in Low Earth Orbit (LEO). During its sojourn in LEO, Intelsat 6 is exposed to an unanticipated environment consisting primarily of atomic oxygen, which will subject the unprotected silver interconnects (nominally 12.5 microns thick) on the solar panel to oxidation and erosion. Rescue by Space Shuttle is being examined. Consequently, Intelsat and Comsat have joined in an effort to determine the condition of the silver interconnects at the anticipated time of reboost and to assess the long term risks to the intended geostationary mission. Ground based tests, theoretical analysis, and a flight experiment aboard STS-41 were executed, and new software was written to calculate the expected total atomic oxygen fluence on the interconnects.
Document ID
19920004040
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
A. Dunnet
(International Telecommunications Satellite Organization Washington, DC, United States)
T.D. Kirkendall
(Communications Satellite Corporation Clarksburg, MD., United States)
Date Acquired
September 6, 2013
Publication Date
August 1, 1991
Publication Information
Publication: ESA, European Space Power Conference. Volume 2: Photovoltaic Generators
Subject Category
Spacecraft Propulsion And Power
Accession Number
92N13258
Distribution Limits
Public
Copyright
Other
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