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USE OF COLD GAS PROPULSION SYSTEM IN A 3U CUBESAT

机译:在3U CUBESAT中使用冷气推进系统

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Cubesats have become quite popular specially among university students as these miniaturized satellites help them in carrying out space exploration feasibly. Till date, cubesats have never flown in space with any well defined propulsion system. But in order to increase mission capabilities like orbit raising and formation flying , or to perform proximity operations , fine attitude control, drag make up and de - orbit without much risks , it is important to use a propulsion system . Here in this paper we have focused on the use of cold gas thrusters in a 3U cubesat.Cold gas thrusters consist of a pressurized tank containing gaseous propellant, such as nitrogen, and a solenoid actuated valve system leading to exit nozzles. Since the propellant is unheated and relies solely on the enthalpy of the stored gas, the velocity at the nozzle exit is relatively low resulting in a low specific impulse, typically around 60 sec, useful for small attitude adjustments and low AV maneuvers. However, the power level, pressure, and weight required in the vessel are though less, but still higher than the Cubesat Specifications provided by the CalPoly. A solution to this problem has been studied and discussed in this paper. Rather than relying on high pressure chambers, we propose the use of solid gas cartridges, which upon ignition by lasers can be released into a chamber containing the gas at a pressure slightly than the atmospheric pressure, from which nitrogen can be drawn for propulsive use. Moreover since only a fraction of the propellant is used for propulsion use, it helps in reducing the tank size and minimizes the risk of leakage and pressure limitations, with reduction in mass by around 20%. This way a suitable propulsion system for a cubesat can be developed which renders increased performance with respect to mission capabilities without increasing the overall mass of the satellite. The idea would also prove to be of much benefit for industries which are planning future cubesat missions.
机译:立方体卫星在大学生中尤其受欢迎,因为这些微型卫星帮助他们切实可行地进行太空探索。迄今为止,立方体卫星从未与任何定义明确的推进系统一起在太空中飞行。但是为了提高任务能力,如提升轨道和编队飞行,或进行近距离作战,精细的姿态控制,阻力弥补和脱离轨道而没有太大的风险,使用推进系统是重要的。在本文中,我们重点介绍了在3U立方体卫星中使用冷气推进器的情况。冷气推进器由装有气态推进剂(例如氮气)的加压罐和通向出口喷嘴的电磁驱动阀系统组成。由于推进剂未加热且仅依赖于所存储气体的焓,因此喷嘴出口处的速度相对较低,导致较低的比冲,通常约为60秒,可用于较小的姿态调整和较低的AV操作。但是,容器中所需的功率水平,压力和重量虽然较小,但仍高于CalPoly提供的Cubesat规格。本文已经研究并讨论了解决该问题的方法。我们建议不要使用高压气室,而是使用固态气瓶,该气瓶在通过激光点火后可以释放到一个装有压力比大气压小的压力的气体的气室中,从中可以抽出氮气进行推进。此外,由于只有一小部分推进剂用于推进,因此有助于减小油箱尺寸并使泄漏和压力限制的风险最小化,质量降低了约20%。这样,可以开发一种适用于立方体卫星的合适的推进系统,该系统在不增加卫星总质量的情况下提高了任务能力的性能。对于正在计划未来的立方体任务的行业,该想法也将证明是非常有益的。

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