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Thermal design considerations for future high-power small satellites

机译:未来大功率小卫星的热设计考虑因素

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High-power Small Satellites have the potential to provide new and advanced capabilities; however, significant challenges prevent wide-spread use. Of these, thermal management of high-heat loads is significant. Although advances in thermal acquisition, transport, and storage are available; thermal dissipation technologies for high-power systems are lacking. Several design concepts are presented focused on high-efficiency, lightweight deployable radiating technologies. Analysis showed that realistic deployable radiator designs offer 220% more thermal dissipation than body-mounted radiator designs, which directly correlates to the same amount of increase in feasible total bus power. Using deployable radiators, a nominal 6U Small Satellite can realistically dissipate around 200 W.
机译:大功率小卫星有潜力提供新的和高级功能;但是,重大挑战可以防止广泛使用。其中,高热负荷的热管理是显着的。虽然热采集,运输和储存的进步是可用的;缺乏高功率系统的热耗散技术。提出了几种设计概念,专注于高效率,轻巧的可部署辐射技术。分析表明,现实的可散散散热器设计提供220%的热耗散,而不是车身散热器设计,其直接与可行总线功率的相同增加的增加量。使用可展开的散热器,标称6U小型卫星可以在200 W左右的现实散发出来。

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