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Radioisotope Thermoelectric Generator Waste Heat System for the Cassini Propulsion Module

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dc.contributor.author Mireles, V. en_US
dc.contributor.author Stultz, J. W. en_US
dc.date.accessioned 2004-10-04T22:36:26Z
dc.date.available 2004-10-04T22:36:26Z
dc.date.issued 1994--June en_US
dc.identifier.citation Friedrichshafen, Germany en_US
dc.identifier.clearanceno 94-0183 en_US
dc.identifier.uri http://hdl.handle.net/2014/32444
dc.description Complete article can be located in Library Journal Stacks SAE 1994 Transactions Journal of Aerospace en_US
dc.description.abstract This paper describes the Radioisotope Thermoelectric Generator (RTG) waste heat system; its development, performance, and effectiveness at controlling the temperatures for the propulson module for the Cassini spacecraft. en_US
dc.format.extent 140201 bytes
dc.format.mimetype application/pdf
dc.language.iso en_US
dc.subject.other Cassini Saturn electrical power propulsion module thermal design en_US
dc.title Radioisotope Thermoelectric Generator Waste Heat System for the Cassini Propulsion Module en_US


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