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New SPIS capabilities to simulate dust electrostatic charging, transport, and contamination of lunar probes

Research output: Contribution to Journal/Magazine › Journal article › peer-review

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New SPIS capabilities to simulate dust electrostatic charging, transport, and contamination of lunar probes. / Hess, S. L. G.; Sarrailh, P.; Matéo-Vélez, J.-C. et al.
In: IEEE Transactions on Plasma Science, Vol. 43, No. 9, 09.09.2015, p. 2799-2807.

Research output: Contribution to Journal/Magazine › Journal article › peer-review

Harvard

Hess, SLG, Sarrailh, P, Matéo-Vélez, J-C, Jeanty-Ruard, B, Cipriani, F, Forest, J, Hilgers, A, Honary, F, Thiébault, B, Marple, S & Rodgers, A 2015, 'New SPIS capabilities to simulate dust electrostatic charging, transport, and contamination of lunar probes', IEEE Transactions on Plasma Science, vol. 43, no. 9, pp. 2799-2807. https://doi.org/10.1109/TPS.2015.2446199

APA

Hess, S. L. G., Sarrailh, P., Matéo-Vélez, J.-C., Jeanty-Ruard, B., Cipriani, F., Forest, J., Hilgers, A., Honary, F., Thiébault, B., Marple, S., & Rodgers, A. (2015). New SPIS capabilities to simulate dust electrostatic charging, transport, and contamination of lunar probes. IEEE Transactions on Plasma Science, 43(9), 2799-2807. https://doi.org/10.1109/TPS.2015.2446199

Vancouver

Hess SLG, Sarrailh P, Matéo-Vélez JC, Jeanty-Ruard B, Cipriani F, Forest J et al. New SPIS capabilities to simulate dust electrostatic charging, transport, and contamination of lunar probes. IEEE Transactions on Plasma Science. 2015 Sept 9;43(9):2799-2807. doi: 10.1109/TPS.2015.2446199

Author

Hess, S. L. G. ; Sarrailh, P. ; Matéo-Vélez, J.-C. et al. / New SPIS capabilities to simulate dust electrostatic charging, transport, and contamination of lunar probes. In: IEEE Transactions on Plasma Science. 2015 ; Vol. 43, No. 9. pp. 2799-2807.

Bibtex

@article{a3009a82e8144285bb153746cdd218f0,
title = "New SPIS capabilities to simulate dust electrostatic charging, transport, and contamination of lunar probes",
abstract = "The spacecraft-plasma interaction simulator has been improved to allow for the simulation of lunar and asteroid dust emission, transport, deposition, and interaction with a spacecraft on or close to the lunar surface. The physics of dust charging and of the forces that they are subject to has been carefully implemented in the code. It is both a tool to address the risks faced by lunar probes on the surface and a tool to study the dust transport physics. We hereby present the details of the physics that has been implemented in the code as well as the interface improvements that allow for a user-friendly insertion of the lunar topology and of the lander in the simulation domain. A realistic case is presented that highlights the capabilities of the code as well as some general results about the interaction between a probe and a dusty environment.",
author = "Hess, {S. L. G.} and P. Sarrailh and J.-C. Mat{\'e}o-V{\'e}lez and B. Jeanty-Ruard and F. Cipriani and J. Forest and A. Hilgers and Farideh Honary and B. Thi{\'e}bault and Steven Marple and A. Rodgers",
note = "Project code: PYA7501",
year = "2015",
month = sep,
day = "9",
doi = "10.1109/TPS.2015.2446199",
language = "English",
volume = "43",
pages = "2799--2807",
journal = "IEEE Transactions on Plasma Science",
issn = "0093-3813",
publisher = "IEEE-INST ELECTRICAL ELECTRONICS ENGINEERS INC",
number = "9",

}

RIS

TY - JOUR

T1 - New SPIS capabilities to simulate dust electrostatic charging, transport, and contamination of lunar probes

AU - Hess, S. L. G.

AU - Sarrailh, P.

AU - Matéo-Vélez, J.-C.

AU - Jeanty-Ruard, B.

AU - Cipriani, F.

AU - Forest, J.

AU - Hilgers, A.

AU - Honary, Farideh

AU - Thiébault, B.

AU - Marple, Steven

AU - Rodgers, A.

N1 - Project code: PYA7501

PY - 2015/9/9

Y1 - 2015/9/9

N2 - The spacecraft-plasma interaction simulator has been improved to allow for the simulation of lunar and asteroid dust emission, transport, deposition, and interaction with a spacecraft on or close to the lunar surface. The physics of dust charging and of the forces that they are subject to has been carefully implemented in the code. It is both a tool to address the risks faced by lunar probes on the surface and a tool to study the dust transport physics. We hereby present the details of the physics that has been implemented in the code as well as the interface improvements that allow for a user-friendly insertion of the lunar topology and of the lander in the simulation domain. A realistic case is presented that highlights the capabilities of the code as well as some general results about the interaction between a probe and a dusty environment.

AB - The spacecraft-plasma interaction simulator has been improved to allow for the simulation of lunar and asteroid dust emission, transport, deposition, and interaction with a spacecraft on or close to the lunar surface. The physics of dust charging and of the forces that they are subject to has been carefully implemented in the code. It is both a tool to address the risks faced by lunar probes on the surface and a tool to study the dust transport physics. We hereby present the details of the physics that has been implemented in the code as well as the interface improvements that allow for a user-friendly insertion of the lunar topology and of the lander in the simulation domain. A realistic case is presented that highlights the capabilities of the code as well as some general results about the interaction between a probe and a dusty environment.

U2 - 10.1109/TPS.2015.2446199

DO - 10.1109/TPS.2015.2446199

M3 - Journal article

VL - 43

SP - 2799

EP - 2807

JO - IEEE Transactions on Plasma Science

JF - IEEE Transactions on Plasma Science

SN - 0093-3813

IS - 9

ER -