Multi-zone kinetic-continuum simulation of an orbit correction thruster back flow around a space station
Gas exhaustion from thrusters mounted on the International Space Station (ISS) is numerically simulated by a multi-zone kinetic-continuum approach. The pressure on the probe located on the ISS is obtained, and comparisons with flight data are performed.
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| creator | Kashkovsky, A. V. Bondar, Ye. A. Krylov, A. N. Rodicheva, A. A. |
| description | Gas exhaustion from thrusters mounted on the International Space Station (ISS) is numerically simulated by a multi-zone kinetic-continuum approach. The pressure on the probe located on the ISS is obtained, and comparisons with flight data are performed. |
| doi_str_mv | 10.1063/5.0187374 |
| format | Conference Proceeding |
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| fulltext | fulltext |
| identifier | ISSN: 0094-243X |
| ispartof | AIP Conference Proceedings, 2024, Vol.2996 (1) |
| issn | 0094-243X 1551-7616 |
| language | eng |
| recordid | cdi_scitation_primary_10_1063_5_0187374 |
| source | AIP Journals Complete |
| subjects | International Space Station Thrusters |
| title | Multi-zone kinetic-continuum simulation of an orbit correction thruster back flow around a space station |
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