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Titan science return quantification

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dc.contributor.author Weisbin, Charles R.
dc.contributor.author Lincoln, William
dc.date.accessioned 2016-06-06T19:02:26Z
dc.date.available 2016-06-06T19:02:26Z
dc.date.issued 2014-08-19
dc.identifier.citation 23rd International Conference On Systems Engineering, Las Vegas, Nevada, August 19-21, 2014 en_US
dc.identifier.clearanceno 14-1133
dc.identifier.uri http://hdl.handle.net/2014/45517
dc.description.abstract Each proposal for a NASA mission concept includes a Science Traceability Matrix (STM), intended to show that what is being proposed would contribute to satisfying one or more of the agency’s top-level science goals. But the information traditionally provided cannot be used directly to quantitatively compare anticipated science return. We added numerical elements to NASA’s STM and developed a software tool to process the data. We then applied this methodology to evaluate a group of competing concepts for a proposed mission to Saturn’s moon, Titan. en_US
dc.description.sponsorship NASA/JPL en_US
dc.language.iso en_US en_US
dc.publisher Pasadena, CA : Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2014 en_US
dc.subject science traceability en_US
dc.subject Saturn en_US
dc.title Titan science return quantification en_US
dc.type Preprint en_US


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