Theoretical and Experimental Research on Microwave Plasma Thruster With Coaxial Resonant Cavity
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Theoretical and Experimental Research on Microwave Plasma Thruster With Coaxial Resonant Cavity
Vol. 19, Issue 4, (2004)
作者机构:
西北工业大学航天学院,陕西,西安,710072
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Published:2004
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TANG Jin-lan, HE Hong-qing, MAO Gen-wang, et al. Theoretical and Experimental Research on Microwave Plasma Thruster With Coaxial Resonant Cavity[J]. 2004, 19(4).
DOI:
TANG Jin-lan, HE Hong-qing, MAO Gen-wang, et al. Theoretical and Experimental Research on Microwave Plasma Thruster With Coaxial Resonant Cavity[J]. 2004, 19(4).DOI:
Theoretical and Experimental Research on Microwave Plasma Thruster With Coaxial Resonant Cavity
The system construction and resonance mode of 100 W power Microwave Plasma Thruster (MPT) With Coaxial Resonant Cavity are introduced.The Resonant Cavity is an important part in the MPT system in which the microwave energy is absorbed by the working gas.In this paper
the numerical simulation of the coupling between microwave energy and plasma flow under the resonant state was analyzed using a coupled Maxwell
Saha and Navier-Stokes solver and the performance of prototype was calculated.All results show that the system principles of 100 W MPT are feasible and the performance of prototype is good.