DocumentCode
1229631
Title
Capacity Charging Circuits for Space Systems Using Silicon-Controlled Rectifiers
Author
Ellern, Felix
Author_Institution
Power Conversion Systems Division Republic Aviation Corporation
Volume
2
Issue
2
fYear
1964
fDate
4/1/1964 12:00:00 AM
Firstpage
505
Lastpage
508
Abstract
Silicon-controlled rectifiers were used in a capacity charging circuit for applications in space where high efficency and low weight are major considerations. This charger can be used to pulse lasers, plasma propulsion engines, sonar, or some thermonuclear devices. The system was compared to conventional designs and found to be particularly advantageous when the discharge rate was varied, or when the ratio of the capacitor charging period to the supply voltage period was high.
Keywords
Capacitors; Circuits; Engines; Optical pulses; Plasma applications; Plasma devices; Propulsion; Rectifiers; Sonar; Space charge;
fLanguage
English
Journal_Title
Aerospace, IEEE Transactions on
Publisher
ieee
ISSN
0536-1516
Type
jour
DOI
10.1109/TA.1964.4319631
Filename
4319631
Link To Document