A summary of the main features and performance of the Spacebus electrical power conditioning system is presented. The subsystems consist of two nickel hydrogen batteries, and a rigid 3W solar array made up of honeycomb carbon fiber panels. The system was used on the Eutelsat 2 spacecraft since 1989. The unique characteristics of this system, especially as regards compatibility to its telecommunications payloads, are outlined.
Spacebus Power Conditioning Application to the Eutelsat 2 Spacecraft
1989
9 pages
Report
No indication
English
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