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
Link To Document :
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