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The ATS-6 power system - Hardware implementation and orbital performanceThe Applications Technology Satellite-6 has performed more than 20 communications, technological and scientific experiments in 2 years of highly successful operation. Contributing substantially to this success has been the flexibility of the power system that allows multiple operation of experiments. The power system, a shunt-boost configuration, uses partial shunt regulation of the solar array and a boost regulator for control of battery power. Regulation is provided for three different operating modes: shunt, charge, and boost. This configuration achieves the highest efficiency of power transfer from the solar array to the loads. The solar array degradation (18.5 percent) has been less than the predicted 20 percent in spite of extreme cycling from -160 C to 60 C. A unique battery cycling regime of discharges varying from 5 percent to 60 percent daily is being encountered. During the second year, noneclipse discharges have occurred twice a day to depths of 35 percent and 45 percent. Battery performance has been good with only a small decrease in end-of-discharge voltage.
Document ID
19770029979
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Lavigna, T. A.
(NASA Goddard Space Flight Center Greenbelt, Md., United States)
Hornbuckle, F. L.
(Fairchild Space and Electronics Co. Germantown, Md., United States)
Date Acquired
August 8, 2013
Publication Date
January 1, 1976
Subject Category
Spacecraft Propulsion And Power
Meeting Information
Meeting: Conference on Intersociety Energy Conversion Engineering
Location: State Line, NV
Start Date: September 12, 1976
End Date: September 17, 1976
Accession Number
77A12831
Distribution Limits
Public
Copyright
Other

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