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MICRO-THRUSTER: 作品数：7被引量：6H指数：2; 导出分析报告; 相关期刊：《航空动力学报》《Chinese Physics B》《Transactions of Nanjing University of Aeronautics and Astronautics》《Plasma Science and Technology》更多>>; 相关基金：国家自然科学基金更多>>

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Effect of Pressure Level on the Performance of an Auto-Initiated Pulsed Plasma Thruster: 《Plasma Science and Technology》2010年第4期466-472,共7页Kelvin LOH Abhijit KUSHARI; funded by ISRO-IITK Space Technology Cell; Pulsed plasma thrusters （PPT） are micro-propulsion devices used in satellites for station keeping. Conventionally the plasma discharge in a PPT is initiated by a spark plug. The primary objective of the present work...; 关键词：plasma thruster auto-initiation solid propellant MICRO-THRUSTER