Raytheon Dual-Use Cryocooler system development

被引:0
|
作者
Hon, R. C. [1 ]
Kirkconnell, C. S. [1 ]
Roberts, T. [2 ]
机构
[1] Raytheon Space & Airborne Syst, El Segundo, CA 90245 USA
[2] Air Force Res Lab, VSSS, Kirtland AFB, NM 87117 USA
来源
ADVANCES IN CRYOGENIC ENGINEERING, VOLS 53A AND 53B | 2008年 / 985卷
关键词
cryocooler; tactical cryocooler; space cryocooler; pulse tube; Stirling; cryocooler electronics;
D O I
暂无
中图分类号
O414.1 [热力学];
学科分类号
摘要
The Dual-Use Cryocooler system, consisting of a single-stage pulse tube thermo-mechanical unit (TMU) in combination with a modified, high reliability set of tactical cryocooler electronics, has been designed to fill the gap that exists between present low-cost tactical and high-cost space cryocooler products. The TMU portion of the system contains a significantly smaller number of parts than typical space cryocoolers while maintaining all of the long-fife features that allow those machines to operate continuously and reliably for 10+ years. This reduction in mechanical complexity positively impacts both unit cost and required build time. The drive electronics have been developed in parallel, and include such features as dual independent motor drives, output waveform shaping, and a variety of TMU / electronics protection algorithms. The fabrication and test cycles for the brassboard system have been completed, and insights gained from these exercises are presented in this paper. Initial design trades and present design status for the TMU and drive electronics are both presented, as well as a comparison of expected versus measured performance. Lastly, an overview of the steps required to bring this system design to flight-readiness will be given.
引用
收藏
页码:538 / +
页数:2
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