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Catenary Model of InSight SEIS Tether for Instrument Deployment

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dc.contributor.author Sorice, Cristina E
dc.contributor.author Bailey, Philip
dc.contributor.author Trebi-Ollennu, Ashitey
dc.contributor.author Kim, Won S
dc.contributor.author Myint, Steven
dc.date.accessioned 2021-03-01T19:08:46Z
dc.date.available 2021-03-01T19:08:46Z
dc.date.issued 2020-03-07
dc.identifier.citation IEEE Aerospace 2020, Big Sky, Montana, March 7-14, 2020
dc.identifier.clearanceno CL#20-0024
dc.identifier.uri http://hdl.handle.net/2014/51123
dc.description.abstract This paper will discuss the motivation and details of the implementation of the SEIS tether model and the ways in which the SEIS tether impacted placement accuracy in certain configurations. It will also show results from testing this model on Earth and deploying SEIS to the Martian surface on sol 22 of InSight’s mission.
dc.description.sponsorship NASA/JPL en_US
dc.language.iso en_US
dc.publisher Pasadena, CA: Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2020
dc.title Catenary Model of InSight SEIS Tether for Instrument Deployment
dc.type Preprint


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