2005
DOI: 10.1117/12.618318
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Performance demonstration of hydrogen advanced loop heat pipe for 20-30K cryocooling of far infrared sensors

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Cited by 8 publications
(4 citation statements)
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“…An optimization of the system to minimize its mass and volume was performed for future space applications, and further results were reported in Ref. [11]. Of particular note that all CLHPs introduced in Refs.…”
Section: Introductionmentioning
confidence: 99%
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“…An optimization of the system to minimize its mass and volume was performed for future space applications, and further results were reported in Ref. [11]. Of particular note that all CLHPs introduced in Refs.…”
Section: Introductionmentioning
confidence: 99%
“…Of particular note that all CLHPs introduced in Refs. [8][9][10][11] employed auxiliary loops to realize the large temperature drop of the primary evaporator during the supercritical startup process, and this method has a good effect in both terrestrial and space surroundings. Refs.…”
Section: Introductionmentioning
confidence: 99%
“…An important example for the CLHP applications is in the thermal control of the space infrared exploration system where the infrared sensors/detectors have to be maintained at 80-100 K or even lower temperatures [14,15].…”
Section: Introductionmentioning
confidence: 99%
“…The CLHP could realize the supercritical startup with a heat load of 2.5W applied to the secondary evaporator when the shroud temperature was 200K; however, a supercritical startup failure occurred in a 298K environment due to large parasitic heat load. The CLHP could operate at a temperature range of 20-30K, and a maximum heat transport capability of 10W over a transport distance of 2.5m was obtained with a 80K shroud [15]. To solve important problems in cryogenic integration, Bugby et al [24,25] developed three CLHPs: an across-gimbal CLHP, a short and a long transport length miniaturized CLHP.…”
Section: Introductionmentioning
confidence: 99%