JPL Technical Report Server

Europa spacecraft configuration optimization for the solar powered vehicle

Show simple item record

dc.contributor.author Horner, Matthew D.
dc.contributor.author Eremenko, Alexander
dc.date.accessioned 2019-07-10T15:20:44Z
dc.date.available 2019-07-10T15:20:44Z
dc.date.issued 2016-03-05
dc.identifier.citation IEEE Aerospace Conference, Big Sky, Montana, March 5-12, 2016 en_US
dc.identifier.clearanceno 16-0018
dc.identifier.uri http://hdl.handle.net/2014/46450
dc.description.abstract A mission to Europa has been on the minds of NASA and JPL for many years. After the Galileo mission to Jupiter in the 1990s there have been various proposals for missions to the Jovian moon. The most recent proposal, previously named the Europa Clipper, has gone through numerous iterations of spacecraft configurations on its road to becoming an official NASA project in June of 2015. Most of these configurations included options for either multi-mission radioisotope thermoelectric generators (MMRTGs) or solar power. In 2014, the decision was made to focus on solar arrays as the source for spacecraft power. 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 Europa spacecraft configuration optimization for the solar powered vehicle en_US
dc.type Preprint en_US


Files in this item

This item appears in the following Collection(s)

Show simple item record

Search


Browse

My Account