一种用于微纳卫星的丙烷微推进系统

Journal of Rocket Propulsion(2012)

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Abstract
介绍了一种应用于某微纳卫星的丙烷微推进系统,该推进系统利用换热模块,在不额外消耗星上电能的情况下实现"液-气"的可靠转化,利用自身的稳压模块和控制模块,系统可实现50 mN推力的快速精确控制。通过轻量化设计技术,系统总重仅2.5 kg。
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Key words
liquefied gas,propane,micro and nano satellite,micro propulsion
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