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PowerThe space station requires an increase in power or energy of at least several orders of magnitude compared to previous space missions. With the requirement up in the range of 10 kilowatt hours, this obviiously requires the development of new technology. Although the power area is very well integrated in the spacecraft itself, it represents a diverse set of components necessary for energy conversion, electronics, and energy distribution. Considerable work is ongoing at NASA Lewis in the power devices development area, including transformers, large area solid-state chips, transistors, and fast recovery diodes. This work is oriented toward eventual application to both AC and DC power conversion approaches. In the energy storage area, there are many options available to fit into the space station representing various degrees of risk and leverage combination, such as the near-term integral-pressure-vessel nickel hydrogen battery, an advanced Ni-H2 battery concept, and the regenrative hydrogen-oxygen system utilizing essentially the Shuttle orbiter type of fuel cell.
Document ID
19840010220
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Corbett, R.
(Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Date Acquired
August 11, 2013
Publication Date
February 1, 1984
Publication Information
Publication: NASA. Langley Research Center Space Station Technol., 1983
Subject Category
Launch Vehicles And Space Vehicles
Accession Number
84N18288
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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