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Development of Multi-Utility Spacecraft Charging Analysis Tool (MUSCAT)

Authors :
Muranaka, Takanobu
Hosoda, Satoshi
Kim, Jeong-Ho
Hatta, Shinji
Ikeda, Koichiro
Hamanaga, Takamitsu
Cho, Mengu
Usui, Hideyuki
Ueda, Hiroko O.
Koga, Kiyokazu
Goka, Tateo
Source :
IEEE Transactions on Plasma Science. Oct, 2008, Vol. 36 Issue 5, p2336, 14 p.
Publication Year :
2008

Abstract

A new numerical software package to analyze spacecraft charging, named 'Multi-Utility Spacecraft Charging Analysis Tool' (MUSCAT), has been developed. MUSCAT consists of an integrated graphical user interface tool called 'Vineyard' and the solver. Vineyard enables satellite engineers to compute spacecraft charging with little knowledge of the numerical calculations. Functions include 3-D satellite modeling, parameter input such as material and orbit environment, data transfer, and visualization of numerical results. Fundamental physical processes of charged-particle--surface interaction are included in the solver. These functions enable MUSCAT to analyze spacecraft charging at geostationary orbit, low Earth orbit, and polar Earth orbit (PEO). The numerical solver code is parallelized for high-speed computation, and the algorithm is optimized to achieve analysis of large-scale PEO satellite in the design phase. Variable time steps are also used to calculate the rapid change of the spacecraft body potential and the gradual change of the differential voltage in a single simulation with a practical number of iterations. In this paper, the functionality, algorithms, and simulation examples of MUSCAT are presented. Index Terms--Simulation software, spacecraft charging.

Details

Language :
English
ISSN :
00933813
Volume :
36
Issue :
5
Database :
Gale General OneFile
Journal :
IEEE Transactions on Plasma Science
Publication Type :
Academic Journal
Accession number :
edsgcl.190002747