| Simulation of plasma behavior for medium propellant mass and pulsed energy of small scale pulsed inductive thruster |
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| 作者姓名： | Yuguo CHENG Guangqing XIA |
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| 作者单位： | 1. PLA 91550 Element 41;2. State Key Laboratory of Structural Analysis for Industrial Equipment, Dalian University of Technology;3. Key Laboratory of Advanced Technology for Aerospace Vehicles of Liaoning Province, Dalian University of Technology |
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| 基金项目： | supported by the National Natural Science Foundation of China (Nos. 11675040 and 11702319)； |
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| 摘 要： | The pulsed inductive thruster is characterized of no electrode corruption and wide propellant choice. To give insight into the propulsion mechanism of small scale thruster at different propellant mass(m) and energy(E) levels, the transient Magneto Hydro Dynamics(MHD) method,completed by high temperature thermodynamic and transport, and plasma electrical models, is developed to study argon plasma response under the excitation of current of high rise rate. By calculating the two-dimensional expans...
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| 收稿时间： | 25 December 2018 |
Simulation of plasma behavior for medium propellant mass and pulsed energy of small scale pulsed inductive thruster |
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| Yuguo CHENG,Guangqing XIA.Simulation of plasma behavior for medium propellant mass and pulsed energy of small scale pulsed inductive thruster[J].Chinese Journal of Aeronautics,2020,33(1):176-190. |
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| Institution: | 1. PLA 91550 Element 41, Dalian 116023, China;2. State Key Laboratory of Structural Analysis for Industrial Equipment, Dalian University of Technology, Dalian 116024, China;3. Key Laboratory of Advanced Technology for Aerospace Vehicles of Liaoning Province, Dalian University of Technology, Dalian 116024, China |
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| Abstract: | |
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| Keywords: | Expansion properties Flow field MagnetoHydroDynamics (MHD) method Pulsed inductive plasma Total impulse |
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