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High capacity power systems for spaceCandidate high-power supply systems for future space missions are discussed. Solar cells, particularly made from GaAs materials, are projected to be amenable large arrays that will have a 10 yr lifetime with a 15 percent efficiency at the end. Concentrator arrays using GaAs cells could furnish over 200 W/sq m with 100 suns irradiance. Different battery systems, other than the present low-power NiCd storage systems, will be required, and could be either fuel cell systems or NiH2 batteries. The flywheel also offers promise, especially if integrated within the attitude control system. Solar thermal systems are also possible, featuring SiGe thermocouples, or boron alloys or rare earth calcogenides in thermoelectric generators or thermionic converters equipped with alkali metal elements. Mechanical systems, notably the Brayton cycle engine, offer multihundredwatt performance and higher, with at least 3.5 yr lifetimes. Experimentation is still needed to characterize the power supply interaction with the spacecraft environment and to design efficient and long-lasting radiators if heat engines are implemented.
Document ID
19840029029
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Mullin, J. P.
(NASA Headquarters Washington, DC United States)
Ambrus, J. H.
(NASA Space Energy Conversion Office Washington, DC, United States)
Date Acquired
August 12, 2013
Publication Date
October 1, 1983
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
IAF PAPER 83-421
Report Number: IAF PAPER 83-421
Accession Number
84A11816
Distribution Limits
Public
Copyright
Other

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