JPL Technical Report Server

Analytical Thermal Model Validation For Cassini Radioisotope Thermoelectric Generator

Show simple item record

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


Files in this item

This item appears in the following Collection(s)

Show simple item record

Search


Browse

My Account