New SPIS Capabilities to Simulate Dust Electrostatic Charging, Transport, and Contamination of Lunar Probes

被引：25

作者：

Hess, S. L. G. ^{[1
]}

Sarrailh, P. ^{[1
]}

Mateo-Velez, J. -C. ^{[1
]}

Jeanty-Ruard, B. ^{[2
]}

Cipriani, F. ^{[3
]}

Forest, J. ^{[2
]}

Hilgers, A. ^{[3
]}

Honary, F. ^{[4
]}

Thiebault, B. ^{[2
]}

Marple, S. R. ^{[4
]}

Rodgers, D. ^{[3
]}

机构：

[1] Off Natl Etud & Rech Aerosp, French Aerosp Lab, F-31000 Toulouse, France

[2] Artenum, F-75010 Paris, France

[3] European Space Agcy, European Space Res & Technol Ctr, NL-2201 AZ Noordwijk, Netherlands

[4] Univ Lancaster, Dept Phys, Lancaster LA1 4YW, England

来源：

IEEE TRANSACTIONS ON PLASMA SCIENCE | 2015年 / 43卷 / 09期

关键词：

Electrostatic levitation; lunar dust; surface charging; PLASMA; MODEL;

D O I：

10.1109/TPS.2015.2446199

中图分类号：

O35 [流体力学]; O53 [等离子体物理学];

学科分类号：

070204 ; 080103 ; 080704 ;

摘要：

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.

引用

页码：2799 / 2807

页数：9

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