NASA plans to orbit a permanently manned space station in the late 1990s, which requires development and assembly of a photovoltaic (PV) power source system to supply up to 75 kW of electrical power average during the orbital period. The electrical power requirements are to be met by a combination of PV source, storage, and control elements for the Sun and eclipse periods. The authors discuss the application of power electronics and controls to manage the generation, storage, and distribution of power to meet the station loads, as well as the computer models used for analysis and simulation of the PV power system. The requirements for power source integrated controls to adjust storage charge power during the insolation period current limiting, breaker interrupt current values, and the electrical fault protection approach are defined. Based on these requirements, operating concepts have been defined which then become drivers for specific system and element design.
Power electronic applications for Space Station Freedom
Leistungselektronikanwendungen für die Raumstation Freedom
1990
8 Seiten, 2 Quellen
Conference paper
English
Photovoltaic power for Space Station Freedom
Tema Archive | 1990
|Online Contents | 1993
|British Library Online Contents | 1993
|NTRS | 1991
|Space station freedom growth power requirements
Tema Archive | 1990
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