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Preliminary report on the CTS transient event counter performance through the 1976 spring eclipse seasonThe transient event counter (TEC), senses and counts transients having a voltage rise of greater than five volts in three separate wire harnesses: the attitude control harness, the solar array instrumentation harness and the solar array power harness. The operational characteristics of TEC are defined and the preliminary results obtained through the first 90 days of operation including the spring 1976 eclipse season are presented. The results show that the Communications Technology Satellite was charged to the point where discharges occurred. The discharge induced transients did not cause any anomalous events in spacecraft operation. The data indicate that discharges can occur at any time during the day without preference to any local time quadrant. The number of discharges occurring in the one second sample interval are greater than anticipated. The compilation and review of the data is continuing.
Document ID
19770003174
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Stevens, N. J.
(NASA Lewis Research Center Cleveland, OH, United States)
Levell, R. R.
(NASA Lewis Research Center Cleveland, OH, United States)
Klinect, V. W.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 3, 2013
Publication Date
January 1, 1976
Subject Category
Launch Vehicles And Space Vehicles
Report/Patent Number
NASA-TM-X-73487
E-8879
Report Number: NASA-TM-X-73487
Report Number: E-8879
Meeting Information
Meeting: Spacecraft Charging Conf.
Location: Colorado Springs
Start Date: October 27, 1976
End Date: October 29, 1976
Sponsors: AF
Accession Number
77N10116
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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