DocumentCode
2349045
Title
Power Line Protection Devices in Space Applications
Author
Volpi, Gian Franco
Author_Institution
Thales Alenia Space Italia S.p.A., Vimodrone
fYear
2007
fDate
9-12 Sept. 2007
Firstpage
1636
Lastpage
1640
Abstract
Simple fuses are seldom used on Board of Satellites for power line protections. Besides the obvious consideration that they can not be changed during flight operations, fuse blowing can generate high inductive spikes in the satellite power bus and therefore endanger the operations of other subsystems or units. Active overload protections are therefore the preferred choice in space application. This paper describes a very fast Latching Current Limiter (LCL) that can be placed at power input of any satellite subsystem, providing overload protections without generating dangerous voltage transients. A detailed theoretical analysis of a discrete LCL, followed by experimental characterization on an Elegant Breadboard, will be presented in the paper. A potential Hybrid implementation will lead to a light, flexible, simple and easy to use device.
Keywords
current limiters; electric fuses; power cables; power transmission protection; flight operations; latching current limiter; overload protections; power line protection devices; satellite power bus; satellite subsystem; space applications; voltage transients; Application software; Artificial satellites; Current limiters; Filters; Fuses; Power generation; Protection; Switches; Temperature; Voltage; Latching Current Limiter; Power Lines Protection; Space;
fLanguage
English
Publisher
ieee
Conference_Titel
EUROCON, 2007. The International Conference on "Computer as a Tool"
Conference_Location
Warsaw
Print_ISBN
978-1-4244-0813-9
Electronic_ISBN
978-1-4244-0813-9
Type
conf
DOI
10.1109/EURCON.2007.4400333
Filename
4400333
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