首页> 外文会议>31st AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit July 10-12, 1995/San Diego, CA >Grid design improvements and test philosophy for a cost-effective approach to ion thruster qualification
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Grid design improvements and test philosophy for a cost-effective approach to ion thruster qualification

机译:网格设计改进和测试理念,以经济高效的方式进行离子推进器鉴定

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The development of a grid erosion computer model can produce a cost-effective approach to ion thruster qualification, most especially when confidence in the model has been established as a result of several long duration tests. However, consideration must be given to operating conditions, such as mass utilisation, anode voltage and facility pressure if the test results are to be used to improve and validate the model. This technique of a limited long duration test (2000 hours) and a grid erosion model has been applied to the UK-10 ion thruster on ARTEMIS. The result is a grid set design which is optimised for maximum lifetime based primarily on two 500 hour tests performed previously. The limited long duration test is due to start early in 1996. The advantage of this approach is that the design has been optimised without a major investiment in a test programme, and the output from the test programme will result in further improvements to the model, so giving good confidence in extrapolations of thruster lifetime.
机译:电网侵蚀计算机模型的开发可以产生具有成本效益的离子推进器资格方法,特别是当由于几个长时间测试而建立了模型的信心时,最多。然而,如果要使用测试结果来改善和验证模型,则必须考虑在操作条件下,例如批量利用,阳极电压和设施压力。这种有限的长时间测试(2000小时)和网格侵蚀模型的这种技术已应用于阿尔忒弥斯的英国离子推进器。结果是网格集设计,该设计主要针对先前执行的两个500小时测试的最大寿命优化。有限的持续时间测试是由于1996年初开始。这种方法的优点是设计已经优化了在测试程序中没有重大投资,并且测试程序的输出将导致模型进一步改进,因此,对推进器寿命的外推着良好的信心。

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