DocumentCode
2175414
Title
Intelsat III traveling wave tube power supply
Author
Gruber, Robert
Author_Institution
Eng. Magnetics Div., Gulton Ind., Hawthorne, CA, USA
fYear
1971
fDate
19-20 April 1971
Firstpage
44
Lastpage
49
Abstract
The performance requirements and design approach used to develop the Intelsat III dual TWT power supply are discussed. In addition, final acceptance test performance data are examined. The dual TWT power supply described here provides power regulation and certain control functions for a 0.1 watt (R.F.) driver and a 12 watt (R.F.) power amplifier operating at 4 GHz. The supply operates from a spacecraft bus voltage of 22 to 31 volts and delivers nearly 2 KV to the high power TWT. Switching regulators are used so power dissipation remains low and virtually constant over the entire input voltage range. The supply is encapsulated and weighs 4.0 lbs. in its 10.6" x 2.3" x 3.5" aluminum case.
Keywords
aircraft power systems; artificial satellites; power amplifiers; Intelsat III dual TWT power supply; power amplifier; power dissipation; power regulation; spacecraft bus voltage; switching regulators; traveling wave tube power supply; Arrays; Cathodes; Heating; Power supplies; Space vehicles; Surges; Voltage control;
fLanguage
English
Publisher
ieee
Conference_Titel
Power Electronics Specialists Conference, 1971 IEEE
Conference_Location
Pasadena, CA
ISSN
0275-9306
Type
conf
DOI
10.1109/PESC.1971.7069133
Filename
7069133
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