Multi-zone kinetic-continuum simulation of an orbit correction thruster back flow around a space station

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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Bibliographische Detailangaben
Hauptverfasser: Kashkovsky, A. V., Bondar, Ye. A., Krylov, A. N., Rodicheva, A. A.
Format: Tagungsbericht
Sprache:eng
Schlagworte:
International Space Station
Thrusters
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Beschreibung
Zusammenfassung: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.
ISSN:0094-243X
1551-7616
DOI:10.1063/5.0187374