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The ATS-6 power system: Hardware implementation and orbital performanceThe Applications Technology Satellite-6 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 excellent dynamic regulation and low output impedance of the power system virtually eliminated the problem of subsystem interactions on the power bus due to conducted interference from load current fluctuations. The performance of the power system continues to be excellent. The solar array degradation (18.5 percent) was less than the specified 20 percent in two years 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 was good with only a small decrease in end-of-discharge voltage. A recent test to evaluate capacity gave 12.4 AH (83% of the nominal capacity of 15 AH) after over 1400 battery discharge cycles. A small increase in the end-of-charge voltage has recently occurred necessitating a change in the charge regime to achieve full charge conditions.
Document ID
19770025285
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Lavigna, T. A.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Hornbuckle, F. L.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
September 3, 2013
Publication Date
September 1, 1977
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
G-7703-X10
NASA-TP-1023
Report Number: G-7703-X10
Report Number: NASA-TP-1023
Accession Number
77N32229
Distribution Limits
Public
Copyright
Public Use Permitted.
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