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ATS-6 spacecraft surface treatment for the control of electrical dischargesThe ATS-6 has been subject to potential charges as high as 11,000 volts based on onboard measurements. Thus, special measures were required to protect the spacecraft surface areas, - primarily the Earth Viewing Module, the reflector support truss, and the solar array boom that were specially processed for thermal control - from electrical discharges whose accompanying fields could destroy sensitive receiving circuits. The paper describes thermal blanket grounding criteria and techniques applied to prevent undesired discharge effects, and discusses the disturbance rate from static discharge in orbit.
Document ID
19760028758
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Keiser, B. E.
Date Acquired
August 8, 2013
Publication Date
November 1, 1975
Publication Information
Publication: IEEE Transactions on Electromagnetic Compatibility
Volume: EMC-17
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
76A11724
Funding Number(s)
CONTRACT_GRANT: NAS5-21100
Distribution Limits
Public
Copyright
Other

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