DocumentCode
2243499
Title
A programmable power processor for high power space applications
Author
Lanier Jr., John R. ; Graves, James R. ; Kapustka, Robert E. ; Bush Jr., John R.
Author_Institution
George C. Marshall Space Flight Center, Alabama 35812
fYear
1982
fDate
14-17 June 1982
Firstpage
331
Lastpage
340
Abstract
A Programmable Power Processor (P3) has been developed by NASA/Marshall Space Flight Center for application in future large space power systems. The P3 is capable of operation over a wide range of input voltage (26 to 375 Vdc) and output voltage (24 to 180 Vdc). The peak output power capability is 18 kW (180 V at 100 A). The output characteristics of the P3 can be programmed to any voltage and/or current level within the limits of the processor and may be controlled as a function of internal or external parameters. Seven breadboard P3s and one "flight-type" engineering model P3 have been built and tested both individually and in electrical power systems. The programmable feature allows the P^ to be used in a variety of applications by changing the output characteristics. The tests have been performed for four potential applications, a high voltage battery peak power tracking charger, a 120-V bus regulator, a 30-V bus regulator, and a peak power tracking impedance matching regulator. Test results, including efficiency at various input/output combinations, transient response, and output impedance, are presented. Packaging considerations for the 18 kW are also discussed.
Keywords
Capacitors; Inductors; Power systems; Power transistors; Regulators; Snubbers; Voltage control;
fLanguage
English
Publisher
ieee
Conference_Titel
Power Electronics Specialists conference, 1982 IEEE
Conference_Location
Cambridge, MA, USA
ISSN
0275-9306
Type
conf
DOI
10.1109/PESC.1982.7072424
Filename
7072424
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