The electric power system of the International Space Station-a platform for power technology development
- 7 November 2002
- conference paper
- Published by Institute of Electrical and Electronics Engineers (IEEE)
- Vol. 4 (1095323X) , 47-54
- https://doi.org/10.1109/aero.2000.878364
Abstract
The electrical power system developed for the International Space Station represents the largest space-based power system ever designed and, consequently, has driven some key technology aspects and operational challenges. The full U.S.-built system consists of a 160 V DC primary network, and a more tightly regulated 120 V DC secondary network. Additionally, the U.S. system interfaces with the 28 V system in the Russian segment. The international nature of the Station has resulted in modular converters, switchgear, outlet panels, and other components being built by different countries, with the associated interface challenges. This paper provides details of the architecture and unique hardware developed for the Space Station, and examines the opportunities it provides for further long-term space power technology development, such as concentrating solar arrays and flywheel energy storage systems.Keywords
This publication has 2 references indexed in Scilit:
- Stability of large DC power systems using switching converters, with application to the International Space StationPublished by Institute of Electrical and Electronics Engineers (IEEE) ,2002
- Flywheel technology and potential benefits for aerospace applicationsPublished by Institute of Electrical and Electronics Engineers (IEEE) ,2002