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Operational thermal control of Cassini Titan flybys

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dc.contributor.author Millard, J. M. en_US
dc.contributor.author Luan, T. W. en_US
dc.date.accessioned 2004-09-17T18:57:28Z
dc.date.available 2004-09-17T18:57:28Z
dc.date.issued 2003-07-07 en_US
dc.identifier.citation 33rd International Conference on Environmental Systems en_US
dc.identifier.citation Vancouver, British Columbia, Canada en_US
dc.identifier.clearanceno 02-2583 en_US
dc.identifier.uri http://hdl.handle.net/2014/10545
dc.description.abstract The Cassini spacecraft will fly by Saturn's largest moon, Titan, forty-five times during its science tour. Twenty-five of the flybys will have a relatively low closest approach target altitude in Titan's atmosphere and are of thermal concern. The Thermal Devices Team on the Cassini Project in Mission Operations at the Jet Propulsion Laboratory has designed an operational thermal control strategy for these flybys. The challenge was to provide flyby operational thermal control that enabled science and remained within design limitations and Project constraints. en_US
dc.format.extent 2623615 bytes
dc.format.mimetype application/pdf
dc.language.iso en_US
dc.subject.other Cassini aeroheating Titan flyby thermal analysis en_US
dc.title Operational thermal control of Cassini Titan flybys en_US


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