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Investigation of the Effects of Facility Background Pressure on the Performance and Voltage-Current Characteristics of the High Voltage Hall Accelerator

机译:设施背景压力对高压霍尔加速器性能和电压-电流特性的影响的研究

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The National Aeronautics and Space Administration (NASA) Science Mission Directorate In-Space Propulsion Technology office is sponsoring NASA Glenn Research Center to develop a 4 kW-class Hall thruster propulsion system for implementation in NASA science missions. A study was conducted to assess the impact of varying the facility background pressure on the High Voltage Hall Accelerator (HiVHAc) thruster performance and voltage-current characteristics. This present study evaluated the HiVHAc thruster performance in the lowest attainable background pressure condition at NASA GRC Vacuum Facility 5 to best simulate space-like conditions. Additional tests were performed at selected thruster operating conditions to investigate and elucidate the underlying physics that change during thruster operation at elevated facility background pressure. Tests were performed at background pressure conditions that are three and ten times higher than the lowest realized background pressure. Results indicated that the thruster discharge specific impulse and efficiency increased with elevated facility background pressure. The voltage-current profiles indicated a narrower stable operating region with increased background pressure. Experimental observations of the thruster operation indicated that increasing the facility background pressure shifted the ionization and acceleration zones upstream towards the thruster's anode. Future tests of the HiVHAc thruster are planned at background pressure conditions that are expected to be two to three times lower than what was achieved during this test campaign. These tests will not only assess the impact of reduced facility background pressure on thruster performance, voltage-current characteristics, and plume properties; but will also attempt to quantify the magnitude of the ionization and acceleration zones upstream shifting as a function of increased background pressure.
机译:美国国家航空航天局(NASA)科学任务局太空推进技术办公室正赞助NASA格伦研究中心开发4 kW级霍尔推力推进系统,以在NASA科学任务中实施。进行了一项研究,以评估改变设施背景压力对高压霍尔加速器(HiVHAc)推进器性能和电压电流特性的影响。本研究评估了NASA GRC真空设施5在最低可达到的背景压力条件下的HiVHAc推进器性能,以最佳模拟太空条件。在选定的推进器运行条件下进行了附加测试,以研究和阐明在设施背景压力升高的情况下推进器运行过程中发生的根本物理变化。测试在背景压力条件下进行,该条件比最低实现的背景压力高三到十倍。结果表明,推进器放电比冲和效率随设备背景压力的升高而增加。电压-电流曲线表明随着背景压力的增加,窄的稳定工作区域。对推进器操作的实验观察表明,增加设施背景压力会使上游的电离区和加速区移向推进器的阳极。计划在背景压力条件下对HiVHAc推进器进行未来的测试,预计该压力将比本次测试中获得的压力低两到三倍。这些测试不仅会评估设施背景压力降低对推进器性能,电压-电流特性和羽流特性的影响;但是还会尝试根据上游背景压力来量化上游移动的电离区和加速区的大小。

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