Show simple item record

dc.contributor.authorKivelson, Margaret G.
dc.contributor.authorJia, Xianzhe
dc.contributor.authorLee, Karen A.
dc.contributor.authorRaymond, Carol A.
dc.contributor.authorKhurana, Krishan K.
dc.contributor.authorPerley, Mitchell O.
dc.contributor.authorBiersteker, John B.
dc.contributor.authorBlacksberg, Jordana
dc.contributor.authorCaron, Ryan
dc.contributor.authorCochrane, Corey J.
dc.contributor.authorDawson, Olivia R.
dc.contributor.authorHarris, Camilla D. K.
dc.contributor.authorJones, Jonathan E.
dc.date.accessioned2023-10-03T20:28:16Z
dc.date.available2023-10-03T20:28:16Z
dc.date.issued2023-09-07
dc.identifier.urihttps://hdl.handle.net/1721.1/152366
dc.description.abstractAbstract Global-scale properties of Europa’s putative ocean, including its depth, thickness, and conductivity, can be established from measurements of the magnetic field on multiple close flybys of the moon at different phases of the synodic and orbital periods such as those planned for the Europa Clipper mission. The Europa Clipper Magnetometer (ECM) has been designed and constructed to provide the required high precision, temporally stable measurements over the range of temperatures and other environmental conditions that will be encountered in the solar wind and at Jupiter. Three low-noise, tri-axial fluxgate sensors provided by the University of California, Los Angeles are controlled by an electronics unit developed at NASA’s Jet Propulsion Laboratory. Each fluxgate sensor measures the vector magnetic field over a wide dynamic range (±4000 nT per axis) with a resolution of 8 pT. A rigorous magnetic cleanliness program has been adopted for the spacecraft and its payload. The sensors are mounted far out on an 8.5 m boom to form a configuration that makes it possible to measure the remaining spacecraft field and remove its contribution to data from the outboard sensor. This paper provides details of the magnetometer design, implementation and testing, the ground calibrations and planned calibrations in cruise and in orbit at Jupiter, and the methods to be used to extract Europa’s inductive response from the data. Data will be collected at nominal rates of 1 or 16 samples/s and will be processed at UCLA and delivered to the Planetary Data System in a timely manner.en_US
dc.publisherSpringer Netherlandsen_US
dc.relation.isversionofhttps://doi.org/10.1007/s11214-023-00989-5en_US
dc.rightsCreative Commons Attributionen_US
dc.rights.urihttps://creativecommons.org/licenses/by/4.0/en_US
dc.sourceSpringer Netherlandsen_US
dc.titleThe Europa Clipper Magnetometeren_US
dc.typeArticleen_US
dc.identifier.citationSpace Science Reviews. 2023 Sep 07;219(6):48en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Earth, Atmospheric, and Planetary Sciences
dc.identifier.mitlicensePUBLISHER_CC
dc.eprint.versionFinal published versionen_US
dc.type.urihttp://purl.org/eprint/type/JournalArticleen_US
eprint.statushttp://purl.org/eprint/status/PeerRevieweden_US
dc.date.updated2023-10-01T03:21:32Z
dc.language.rfc3066en
dc.rights.holderThe Author(s)
dspace.embargo.termsN
dspace.date.submission2023-10-01T03:21:32Z
mit.licensePUBLISHER_CC
mit.metadata.statusAuthority Work and Publication Information Neededen_US


Files in this item

Thumbnail

This item appears in the following Collection(s)

Show simple item record