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Air Force Research Laboratory Cryocooler Technology Development

机译:空军研究实验室冷冻室技术开发

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This paper presents an overview of the cryogenic refrigerator and cryogenic integration programs in development and characterization under the Cryogenic Cooling Technology Group, Space Vehicles Directorate of the Air Force Research Laboratory (AFRL). The vision statement for the group is to support the space community as the center of excellence for developing and transitioning space cryogenic thermal management technologies.This paper will describe the range of Stirling, pulse tube; reverse Brayton, and Joule-Thomson cycle cryocoolers currently under development to meet current and future Air Force and Department of Defense requirements. Cooling requirements at 10K, 35K, 60K, 95K, and multistage cooling requirements at 35/85K are addressed. In order to meet these various requirements, the Air Force Research Laboratory, Space Vehicles Directorate is pursuing various strategic cryocooler and cryogenic integration options.The Air Force Research Laboratory, working with industry partners, is also developing several advanced cryogenic integration technologies that will result in the reduction in current cryogenic system integration penalties and design time. These technologies include the continued development of gimbaled transport systems, 35K and 10K thermal storage units, heat pipes, cryogenic straps, and thermal switches.
机译:本文概述了低温冷却技术组下的发育和表征中的低温冰箱和低温集成计划,空间车辆的空军研究实验室(AFRL)。本集团的愿景声明是支持空间社区作为开发和过渡空间低温热管理技术的卓越中心。本文将描述斯特林,脉冲管的范围;逆转布雷顿和若尔汤森循环龙卷风手机正在开发,以满足当前和未来的空军和国防部要求。在35 / 85K时,10K,35K,60K,95K和多级冷却要求的冷却要求得到了解决。为了满足这些各种要求,空军研究实验室,太空车辆局长正在追求各种战略沟槽和低温整合选择。空军研究实验室与行业合作伙伴合作,也在开发几种先进的低温集成技术,将导致减少电流低温系统集成惩罚和设计时间。这些技术包括持续开发万向石运输系统,35K和10K热存储单元,热管,低温带和热开关。

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