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Titlebook: Cryocoolers 11; R. G. Ross Book 2002 Springer Science+Business Media New York 2002 electronics.material.refrigeration.space

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樓主: brachytherapy
51#
發(fā)表于 2025-3-30 11:18:46 | 只看該作者
52#
發(fā)表于 2025-3-30 12:44:17 | 只看該作者
High Reliability Coolers under Development at Signaal-USFAxure-bearing suspension, side loads on the piston seals are avoided. A proper alignment procedure ensures no contact between piston and cylinder during operation, resulting in the absence of wear of the piston coating, which normally determines the lifetime of a cooler..The moving-magnet technology,
53#
發(fā)表于 2025-3-30 19:04:37 | 只看該作者
54#
發(fā)表于 2025-3-30 22:04:29 | 只看該作者
TES FPC Flight Pulse Tube Cooler Systeme coolers are required to provide 1W cooling at 57K while rejecting to 35°C with less than 63W input power to the electronics. The system (cooler and electronics) required mass is less than 17.1 kg. The system also includes radiation-hardened control electronics and provides cooler control functions
55#
發(fā)表于 2025-3-31 03:07:00 | 只看該作者
Pursuing Practice Wisdom in Leadershipily on reliability and the achievement of long life. However, looking ahead at 21 st century military space applications, there are improvements needed in several aspects of current cooling technology including higher capacity cooling loads, mass reduction, and improvement in efficiency, low tempera
56#
發(fā)表于 2025-3-31 08:32:17 | 只看該作者
have low input power, a quick cool-down tune, low vibration output, low audible noise, and higher reliability. This paper (1) outlines the characteristics of each cooler, (2) presents the status and results of qualification tests, and (3) presents the status and test results of efforts to increase
57#
發(fā)表于 2025-3-31 10:19:35 | 只看該作者
58#
發(fā)表于 2025-3-31 15:14:20 | 只看該作者
59#
發(fā)表于 2025-3-31 19:23:33 | 只看該作者
60#
發(fā)表于 2025-4-1 01:16:11 | 只看該作者
Karen Keifer-Boyd,Wanda B. Knight,Ann Holtich uses a mass balancer to reduce vibration. It is designed to lift a heat load of 2W at 60K, with a nominal rejection temperature of 300K. The characterization of the PSC involved a series of experiments, including cool-down to lowest temperature, design point verification, parameter optimization,
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