Energetics of Propellant Options for High-Power Hall Thrusters

机译：大功率霍尔推力器推进剂选择的能量学

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Several propellant options for use in high-power Hall thrusters are analyzed. Krypton,rnCadmium, Iodine, Cesium, Mercury, and Bismuth are analyzed and compared to Xenon in several areas ofrnperformance. Performance parameters examined include thrust, specific impulse, probability of ionization,rnmaximum theoretical efficiency, and sputter yield.

机译：分析了用于大功率霍尔推力器的几种推进剂选项。分析了rypto，镉，碘，铯，汞和铋，并在几个性能方面与氙进行了比较。检查的性能参数包括推力，比冲，电离的概率，最大理论效率和溅射产量。

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来源
《Space nuclear conference 2005 (SNC'05): proceedings of the embedded topical meeting》|2005年|1092-1101|共10页
会议地点 San Diego CA(US);San Diego CA(US)
作者
Alex Kieckhafer; Lyon B. King;
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作者单位

Michigan Technological Universityrn815 R.L. Smith BldgrnHoughton, MI 49931;

Michigan Technological Universityrn815 R.L. Smith BldgrnHoughton, MI 49931;

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1. Performance optimization of a krypton Hall thruster with a rotating propellant supply [J] . Acta astronautica . 2020,第Juna期

机译：具有旋转推进剂供应的Hall霍尔推进器的性能优化
2. Simulation of a Hall Effect Thruster Using Krypton Propellant [J] . Horatiu C. Dragnea, Alejandro Lopez Ortega, Hani Kamhawi, Journal of propulsion and power . 2020,第3期

机译：用rypto推进剂模拟霍尔效应推进器
3. Discharge characteristics and increased electron current during azimuthally nonuniform propellant supply in an anode layer Hall thruster [J] . J. Bak, B. Van Loo, R. Kawashima, Journal of Applied Physics . 2020,第2期

机译：在阳极层霍尔推进器中的方位角不均匀推进剂供应中的放电特性和增加的电子电流
4. Energetics of Propellant Options for High-Power Hall Thrusters [C] . Space nuclear conference . 2005

机译：高功率霍尔推进人的推进剂选择的能量学
5. Clustering of Hall effect thrusters for high-power electric propulsion applications. [D] . Beal, Brian Eric. 2004

机译：适用于大功率电力推进应用的霍尔效应推进器集群。
6. A propellant-free superconducting solenoid thruster driven by geomagnetic field [O] . Heng-Wei Kuo, Kuo-Long Pan, Wei-Li Lee 2021

机译：由地磁场驱动的无推进剂超导螺线管推进器
7. A novel hall thruster utilizing space debris as the propellant [O] . Peng E, Wenbin Ling 2016

机译：利用空间碎片作为推进剂的新颖霍尔推进器

Energetics of Propellant Options for High-Power Hall Thrusters

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