The Simulation of Molecular Return Flux in Thermal Vacuum Test of Spacecraft

Abstract:

In process of thermal vacuum test of spacecraft, the molecular contamination can have severe effects on performance and reliability of optical payload. In this article, we analyzed the contamination transport mechanism, simplified boundary conditions and input parameters based on physical understanding. We employed the Direct Simulation Monte-Carlo method to simulate the return flux of molecular contamination scattered by residual gas molecules in thermal vacuum tests of solar array and whole satellite. The results of simulation show that the return flux cannot be ignored, and its highest value would be 0.004. This would help the contamination control of spacecraft design, manufacture, test, and on-orbit operation.

• Periodical: Applied Mechanics and Materials (Volumes 789-790)
• Pages: 471-476
• DOI: https://doi.org/10.4028/www.scientific.net/AMM.789-790.471
• Online since: September 2015
• Authors: Zi Long Jiao, Li Xiang Jiang, Ji Peng Sun, Jian Guo Huang, Yun Fei Zhu
• Keywords: Direct Simulation Monte-Carlo, Molecular Contamination, Return Flux, Thermal Vacuum Test

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