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First test flight thermal performance of the low density supersonic decelerator (LDSD) supersonic flight dynamics test (SFDT) vehicle

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dc.contributor.author Mastropietro, A.J.
dc.contributor.author Kempenaar, Jason
dc.contributor.author Redmond, Matthew
dc.contributor.author Pauken, Michael
dc.date.accessioned 2017-07-26T16:19:09Z
dc.date.available 2017-07-26T16:19:09Z
dc.date.issued 2015-07-12
dc.identifier.citation 45th International Conference on Environmental Systems, Bellevue, Washington, July 12-16, 2015 en_US
dc.identifier.clearanceno 15-2128
dc.identifier.uri http://hdl.handle.net/2014/45732
dc.description.abstract The thermal telemetry from the first test flight, an assessment of post-flight inspections of the recovered vehicle, and a review of the thermal design and model of the vehicle will be presented along with several lessons learned. 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, 2015 en_US
dc.subject decelerator en_US
dc.subject telemetry en_US
dc.subject flight test data en_US
dc.subject thermal analysis en_US
dc.title First test flight thermal performance of the low density supersonic decelerator (LDSD) supersonic flight dynamics test (SFDT) vehicle en_US
dc.type Presentation en_US


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