用于太空技术7号任务的胶体微牛顿推进器

J. Ziemer, T. Randolph, G. Franklin, V. Hruby, D. Spence, N. Demmons, T. Roy, E. Ehrbar, J. Zwahlen, Roy Martin, W. Connolly
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引用次数: 40

摘要

由四个胶体微牛顿推进器(CMNT)系统组成的两个飞行合格集群已交付给喷气推进实验室(JPL),随后交付给欧空局进行航天器集成。这些集群将为无拖曳技术演示任务“空间技术7号”(ST7)提供精确的航天器控制。ST7任务由美国宇航局新千年计划赞助,将为未来的任务演示精确编队飞行技术,如激光干涉仪空间天线(LISA)任务。ST7干扰减少系统(DRS)是ESA LISA探路者航天器上的有效载荷,与欧洲重力参考传感器(GRS)一起作为ESA LISA技术包(LTP)的一部分。为了实现纳米级精密航天器控制要求,8个推进器系统中的每一个都需要提供5到30µN的推力,分辨率≤0.1µN,推力噪声≤0.1µN/vHz。CMNT由Busek公司开发,在JPL的设计和测试支持下,在过去的六年里,CMNT已经发展成为一个飞行准备和飞行合格的微推进器系统,这是同类系统中的第一个。最近的飞行单元资格测试包括振动和热真空环境测试,以及性能验证和验收测试。在交付给JPL之前,所有测试都已成功完成。首架飞机于2008年2月交付,第二架飞机于2008年5月交付。自抵达喷气推进实验室以来,这些单元已经成功地通过了质量分布、磁性和EMI/EMC测量和测试,作为集成和测试(I&T)活动的一部分,包括集成航空电子设备单元(IAU)。飞行软件序列已经在全飞行DRS仪器的地面测试中成功地进行了测试和验证,包括全功能和72小时自主操作测试。2009年夏天,这些星团组件连同IAU一起被交付给ESA,用于整合到LISA探路者航天器中。航天器级测试将包括磁性、声学和热真空环境测试,并计划在2012年4月进行发射和飞行演示。1 2
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Colloid Micro-Newton Thrusters for the space technology 7 mission
Two flight-qualified clusters of four Colloid Micro-Newton Thruster (CMNT) systems have been delivered to the Jet Propulsion Laboratory (JPL) and subsequently delivered to ESA for spacecraft integration. The clusters will provide precise spacecraft control for the drag-free technology demonstration mission, Space Technology 7 (ST7). The ST7 mission is sponsored by the NASA New Millennium Program and will demonstrate precision formation flying technologies for future missions such as the Laser Interferometer Space Antenna (LISA) mission. The ST7 disturbance reduction system (DRS) is a payload on the ESA LISA Pathfinder spacecraft along with the European gravitational reference sensor (GRS) as part of the ESA LISA Technology Package (LTP). To achieve the nanometer-level precision spacecraft control requirements, each of eight thruster systems is required to provide thrust between 5 and 30 µN with resolution ≤0.1 µN and thrust noise ≤0.1 µN/vHz. Developed by Busek Co. Inc., with support from JPL in design and testing, the CMNT has been developed over the last six years into a flight-ready and flight-qualified microthruster system, the first of its kind. Recent flight-unit qualification tests have included vibration and thermal vacuum environmental testing, as well as performance verification and acceptance tests. All tests have been completed successfully prior to delivery to JPL. Delivery of the first flight unit occurred in February of 2008 with the second unit following in May of 2008. Since arrival at JPL, the units have successfully passed through mass distribution, magnetic, and EMI/EMC measurements and tests as part of the integration and test (I&T) activities including the integrated avionics unit (IAU). Flight software sequences have been tested and validated with the full flight DRS instrument successfully to the extent possible in ground testing, including full functional and 72 hour autonomous operations tests. In the summer of 2009 the cluster assemblies were delivered to ESA along with the IAU for integration into the LISA Pathfinder spacecraft. Spacecraft-level testing will include magnetics, acoustic, and thermal vacuum environmental testing with a planned launch and flight demonstration in April 2012. 1 2
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