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Environmental Testing of NASA's Evolutionary Xenon Thruster Prototype Model 1 Reworked Ion Engine

机译:NASA进化型氙气推进器原型1型重做离子发动机的环境测试

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NASA's Evolutionary Xenon Thruster propulsion system is an advanced ion propulsion system that is oriented toward robotic exploration of the solar system using solar electric power. The subsystem includes an ion engine, a power processing unit, feed system components, and a thruster gimbal. The prototype model engine, PM1, was subjected to qualification-level environmental testing to demonstrate compatibility with environments representative of anticipated mission requirements. Although the testing was largely successful, several issues were identified, including the fragmentation of potting cement on the discharge and neutralizer cathode heater terminations during vibration, which led to abbreviated thermal testing, and the generation of particulate contamination from manufacturing processes and engine materials. The engine was reworked to address most of these findings and renamed PM1R, and the environmental test sequence was repeated. Thruster functional testing was performed before and after the vibration and thermal-vacuum tests. Random vibration testing, conducted with the thruster mated to the breadboard gimbal, was executed at 10.0 g_(rms) for 2 min in each of the three axes. Thermal-vacuum testing included three thermal cycles from -120 to 215℃ with hot engine restarts. Thruster performance was nominal throughout the test program, with minor variations in a few engine operating parameters likely caused by facility effects. There were no significant changes in engine performance as characterized by the engine operating parameters, ion optics performance measurements, and beam current density measurements, indicating no significant changes to the hardware as a result of the environmental testing. The redesigned cathode heater terminations successfully survived the vibration environments. NASA's Evolutionary Xenon Thruster PM1R engine and the breadboard gimbal were found to be well designed to meet environmental requirements based on the results reported herein.
机译:NASA的“进化氙气推进器”推进系统是一种先进的离子推进系统,旨在利用太阳能发电对机器人进行自动探测。子系统包括离子引擎,功率处理单元,进料系统组件和推进器万向架。原型模型引擎PM1经过了资格级别的环境测试,以证明与代表预期任务要求的环境的兼容性。尽管测试取得了很大的成功,但仍发现了一些问题,包括振动过程中放电和中和器阴极加热器端子上的灌封胶破碎,从而导致了简化的热测试,以及制造过程和发动机材料中产生的微粒污染。对该引擎进行了重新设计以解决这些发现中的大部分问题,并将其重命名为PM1R,并重复了环境测试程序。在振动和热真空测试之前和之后进行推进器功能测试。在推进器与面包板万向架配合的情况下,在三个轴中的每一个轴上以10.0 g_(rms)进行了2分钟的随机振动测试。热真空测试包括从-120至215℃的三个热循环,并重新启动发动机。在整个测试程序中,推力器的性能都是正常的,一些发动机运行参数的细微变化很可能是由设施影响引起的。以发动机运行参数,离子光学性能测量和电子束电流密度测量为特征的发动机性能没有显着变化,这表明环境测试没有对硬件造成显着变化。重新设计的阴极加热器终端成功地经受住了振动环境的影响。根据本文报告的结果,发现NASA的Evolution Xenon Thruster PM1R发动机和面包板万向架经过精心设计,可以满足环境要求。

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  • 来源
    《Journal of propulsion and power》 |2009年第1期|94-104|共11页
  • 作者单位

    Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California 91109 Electric Propulsion Group, 4800 Oak Grove Dr., Mail Stop 125-109;

    Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California 91109 Electric Propulsion Group, 4800 Oak Grove Dr., Mail Stop 125-109;

    NASA John H. Glenn Research Center at Lewis Field,Cleveland, Ohio 44135 Propulsion and Propellants Branch, 21000 Brookpark Road, Mail Stop 16-1;

    NASA John H. Glenn Research Center at Lewis Field,Cleveland, Ohio 44135 Propulsion and Propellants Branch, 21000 Brookpark Road, Mail Stop 16-1;

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