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V&V on a NASA technology demonstration project: low density supersonic decelerator

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dc.contributor.author Murry, Michael L.
dc.contributor.author Randolph, Thomas M.
dc.date.accessioned 2019-07-10T15:21:51Z
dc.date.available 2019-07-10T15:21:51Z
dc.date.issued 2016-03-05
dc.identifier.citation IEEE Aerospace Conference, Big Sky, Montana, March 5-12, 2016 en_US
dc.identifier.clearanceno 16-0035
dc.identifier.uri http://hdl.handle.net/2014/46453
dc.description.abstract Given their smaller budgets, but higher allowed risk posture, technology demonstration missions face different Verification and Validation (V&V) challenges than typical NASA missions. Despite these challenges, the Low Density Supersonic Decelerator (LDSD) project, managed by NASA’s Jet Propulsion Laboratory (JPL), has been extremely successful in testing new supersonic atmospheric decelerator technologies. A contribution to the project’s success is the unique V&V program that emphasized efficiency and flexibility. This paper will provide an overview of LDSD test objectives, Supersonic Flight Dynamics Tests (SFDT) performed so far, unique requirements structure and V&V processes implemented. The paper will focus on the V&V of the SFDT test architecture. Furthermore, lessons learned will also be presented at the end of the paper to aid future technology demonstration projects. 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, 2016 en_US
dc.title V&V on a NASA technology demonstration project: low density supersonic decelerator en_US
dc.type Preprint en_US


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