Analytical Thermal Model Validation For Cassini Radioisotope Thermoelectric Generator

Lin, Edward I.

dc.contributor.author	Lin, Edward I.	en_US
dc.date.accessioned	2004-09-26
dc.date.available	2004-09-26
dc.date.issued	1997-07-27	en_US
dc.identifier.citation	Honolulu, Hawaii, USA	en_US
dc.identifier.clearanceno	97-0765	en_US
dc.identifier.uri	http://hdl.handle.net/2014/22291
dc.description.abstract	The Saturn-bound cassini spacecraft is designed to rely, without precedent, on the waste heat from its three radioisotope thermoelectric generators (RTGs) to warm the propulsion module sybsystem, and the RTG end dome temperature is a key determining factor of the amount of waste heat delivered.	en_US
dc.format.extent	347938 bytes
dc.format.mimetype	application/pdf
dc.language.iso	en_US
dc.subject.other	Cassini Radioisotope Thermoelectric Generator	en_US
dc.title	Analytical Thermal Model Validation For Cassini Radioisotope Thermoelectric Generator	en_US