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Titlebook: Cryocoolers 10; R. G. Ross Book 2002 Springer Science+Business Media New York 2002 Motor.Simulation.alloy.design.development.electronics.m

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Multispectral Thermal Imager (MTI) Space Cryocooler Development, Integration, and Testf cooling at 60 Kelvin. The focal plane is under development at Santa Barbara Research Center (SBRC). Both items are one-of-kind products whose integration occurs in the later phases of the MTI system build, thereby posing potential schedule risks to the overall program success. The existence of a T
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An Overview of the Performance and Maturity of Long Life Cryocoolers for Space Applicationsion types. These coolers range in capacities from a few milliwatts to over 10 W at temperatures from 10 K to over 120 K and include single and multi-stage designs. The primary objectives of this study were to provide a hardware summary and performance comparison for potential space cryocooler users
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DARPA Low Cost Cryocooler Performance Testing: Preliminary Resultsces offer significantly enhanced performance at cryogenic temperatures compared to ambient temperature operation. There have been few commercial or industrial products that exploit cryogenic temperature operation due to the cost and reliability of cryocooling system. To address this cryocooling need
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Qualification Test Results for a Dual-Temperature Stirling Cryocooleret requirements such as power efficiency, compatibility with sensitive instruments, and high reliability. In this work we discuss a cooler tailored to efficiently provide refrigeration at two different temperatures simultaneously. This protoflight maturity-level cooler delivers approximately 0.4 W o
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