SPIS simulations with and without the thruster from 0.067 AU to 1 AU

Access status:

Open Access

Field	Value	Language
dc.contributor.author	Shinde, Tejaswi
dc.coverage.spatial	University of Sydney	en_AU
dc.coverage.temporal	7, 2023	en_AU
dc.date.accessioned	2023-12-08T05:07:25Z
dc.date.available	2023-12-08T05:07:25Z
dc.date.issued	2023-12-08
dc.identifier.uri	https://hdl.handle.net/2123/31951
dc.description.abstract	The 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_AU
dc.language.iso	en	en_AU
dc.rights	Creative Commons Attribution 4.0	en_AU
dc.subject	Spacecraft charging	en_AU
dc.subject	Ion induced charging	en_AU
dc.title	SPIS simulations with and without the thruster from 0.067 AU to 1 AU	en_AU
dc.type	Dataset	en_AU
dc.subject.asrc	ANZSRC FoR code::51 PHYSICAL SCIENCES	en_AU
dc.identifier.doi	10.25910/vv3g-zr19
dc.description.method	The data was extracted from the SPIS simulation output folder and then analysed using the Microsoft Excel.	en_AU
usyd.faculty	SeS faculties schools::Faculty of Science	en_AU
usyd.department	Department of Physics	en_AU
workflow.metadata.only	No	en_AU