Paper
15 October 2004 Numerical modeling of ISS thruster plume induced contamination environment
Alina A. Alexeenko, Dean C. Wadsworth, Sergey F. Gimelshein, Andrew D. Ketsdever
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Abstract
The molecular and liquid droplet thruster-induced contamination is studied numerically for a 130 N ISS bipropellant thruster using Navier-Stokes and DSMC flow solvers and a Lagrangian particle tracking. The molecular sources contributing to the inorganic components of the plume backflow contaminant are estimated, and a qualitative characterization of the liquid droplet contribution to the organic part of contaminant is conducted. The total calculated mass flux of the molecular contaminant in the backflow region compares very well with the experimental measurement on-board of Mir space station. The computations show that approximately 20 to 30 per cent of the droplets formed at the break up of the unburned propellant film at the exit can contribute to the organic part of the backflow contaminant.
© (2004) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
Alina A. Alexeenko, Dean C. Wadsworth, Sergey F. Gimelshein, and Andrew D. Ketsdever "Numerical modeling of ISS thruster plume induced contamination environment", Proc. SPIE 5526, Optical Systems Degradation, Contamination, and Stray Light: Effects, Measurements, and Control, (15 October 2004); https://doi.org/10.1117/12.559059
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Cited by 14 scholarly publications.
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KEYWORDS
Contamination

Liquids

Laser induced plasma spectroscopy

Molecules

Numerical modeling

Particles

Monte Carlo methods

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