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1. 发明申请

WO2017176310A1 SATELLITE WITH INTEGRAL THRUSTERS 审中-公开
标题翻译：带有整体推力器的卫星
公开(公告)号：WO2017176310A1
公开(公告)日：2017-10-12
申请号：PCT/US2016/056382
申请日：2016-10-11
申请人： RAYTHEON COMPANY
发明人： KOEHLER, Frederick, B. , DANFORTH, Jeremy, C. , LYMAN, Ward, D. , LANGHENRY, Mark, T. , SUMMERS, Matt, H. , PONTIUS, Paul, E. , PAPE, Brian, M. , STALLINGS, Jared, D. , VILLARREAL, James, K. , VILLARREAL, Thomas
IPC分类号： B64G1/10 , B64G1/40
摘要： A satellite (10) has thrusters (18) that are integral parts of its frame (12). The frame defines cavities therein where thrusters are located. The thrusters may include an electrically-operated propellant and electrodes to activate combustion in the electrically-operated propellant. The frame may be additively manufactured, and the propellant and/or the electrodes may also be additively manufactured, with the frame and the propellant and/or the electrodes also being manufactured in a single process. In addition the thrusters may have nozzle portions through which combustion gases exit the thrusters. The thrusters may be located at corners and/or along edges of the frame, and may be used to accomplish any of a variety of maneuvers for the satellite. The satellite may be a small satellite, such as a CubeSat satellite, for instance having a volume of about 1 liter, and a mass of no more than about 1.33 kg.
摘要翻译：卫星（10）具有作为其框架（12）的组成部分的推进器（18）。框架限定推进器所在的空腔。推进器可以包括电驱动推进剂和电极以激活电驱动推进剂中的燃烧。框架可以加成制造，并且推进剂和/或电极也可以附加地制造，其中框架和推进剂和/或电极也可以在单个工艺中制造。另外，推进器可具有喷嘴部分，燃烧气体通过喷嘴部分离开推进器。推进器可以位于框架的角落和/或沿着框架的边缘，并且可以用于完成卫星的各种操纵中的任何一种。卫星可以是小卫星，例如CubeSat卫星，例如具有约1升的体积和不大于约1.33kg的质量。

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