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dc.contributor.authorShinde, Tejaswi
dc.coverage.spatialUniversity of Sydneyen
dc.coverage.temporal7, 2023en
dc.date.accessioned2023-12-08T05:07:25Z
dc.date.available2023-12-08T05:07:25Z
dc.date.issued2023-12-08
dc.identifier.urihttps://hdl.handle.net/2123/31951
dc.description.abstractThe file includes raw data extracted from the SPIS simulations for two cases a.) with SPT-100 thruster and b.) Without thruster. The plots in the manuscript are generated using this data. Additionally for full reproducibility of the simulation please find the .spis file, .geo and .msh file with and without the thruster at 1AU. Note that for any other location, the simulation files (.spis, .geo and .msh) can be modified using the right environmental parameters.en
dc.language.isoenen
dc.rightsCreative Commons Attribution 4.0en
dc.subjectSpacecraft chargingen
dc.subjectIon induced chargingen
dc.titleSPIS simulations with and without the thruster from 0.067 AU to 1 AUen
dc.typeDataseten
dc.subject.asrcANZSRC FoR code::51 PHYSICAL SCIENCESen
dc.identifier.doi10.25910/vv3g-zr19
dc.description.methodThe data was extracted from the SPIS simulation output folder and then analysed using the Microsoft Excel.en
usyd.facultySeS faculties schools::Faculty of Scienceen
usyd.departmentDepartment of Physicsen
workflow.metadata.onlyNoen


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