Catenary Model of InSight SEIS Tether for Instrument Deployment

Sorice, Cristina E; Bailey, Philip; Trebi-Ollennu, Ashitey; Kim, Won S; Myint, Steven

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