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Advanced Micro-Propulsion based on the Micro-Cathode Arc Thruster

机译:基于微阴极弧推推的先进微型推进器

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The George Washington University developed the Micro-Cathode Arc Thruster pCAT in 2008. The μCAT is an electric propulsion system that is based on the well-researched ablative vacuum arc or 'cathodic arc' process. Due to the physical nature of the arc discharge, any conductive material can be used as a propellant, as long as it is solid. This allows the thruster to operate with different metals, each with different physical properties, giving the mission designer flexibility when it comes to the mission's design. To exemplify this: if a nickel cathode is used, the thrusters will produce a higher thrust compared to titanium, but the latter would offer a higher specific impulse under similar conditions. The system caters to small satellites and is designed mostly for attitude control tasks where small impulse bits are required. The μCAT system has been flown on BRICSat-P, which is a 1.5 U CubeSat mission led by the United States Naval Academy (USNA). Preliminary reports show that the propulsion system was capable of detumbling the satellite to a rate of less than 1 degree per second on all axes within 48 hours of deployment. The system is scheduled to fly on two more missions within the next 12 months. The first mission is Canyval-X, which is a joint project between NASA Goddard Space Flight Center, the Korean space agency KARI, GWU, and the Yonsei University in Korea. The second mission is another partnership with the United States Naval Academy, who will be launching BRICSat-2, a follow-up mission to their previous joint project with GWU, BRICSat-P. Most recently, the Laboratory began work in an advanced version of the system, that will be designed to provide CubeSats with a main propulsion system based on the μCAT system. The new thruster works as a two-stage propulsion system that is designed to accelerate the plasma further, providing higher thrusts and higher specific impulses of over 3000 seconds. The first version of the propulsion system uses an accelerati
机译:乔治华盛顿大学于2008年开发了微观阴极弧推推式PCAT。μCAT是一种电动推进系统,基于研究良好的烧蚀真空弧或“阴极电弧”过程。由于电弧放电的物理性质,任何导电材料都可以用作推进剂,只要它是固体即可。这允许推进器以不同的金属运行,每个金属具有不同的物理性质,在涉及特派团的设计方面提供了任务设计者的灵活性。为了举例说明:如果使用镍阴极,则与钛相比,推动器将产生较高的推力,但后者将在类似条件下提供更高的特定脉冲。系统迎合小型卫星,而且主要用于姿态控制任务,其中需要小脉冲位。 μCAT系统已经在Bricsat-P上飞行,这是美国海军学院(USA)领导的1.5 U CubeSat任务。初步报告表明,推进系统能够在部署48小时内的所有轴上将卫星拆卸到每秒小于1度的速率。该系统计划在未来12个月内在另外两个特派团上飞行。第一个任务是Canyval-X,它是NASA戈达德太空飞行中心,韩国航天局Kari,GWU和韩国延世大学之间的联合项目。第二个任务是与美国海军学院的另一种伙伴关系,他将推出Bricsat-2,这是与GWU,Bricsat-P的以前的联合项目的后续任务。最近,实验室开始在系统的先进版本中工作,这将设计为基于μCAT系统的主要推进系统提供CubeSats。新推进器用作两级推进系统,旨在进一步加速等离子体,提供更高的推力和较高的特定冲动超过3000秒。推进系统的第一个版本使用Accelerati

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