SAE Technical Paper Series 2000
DOI: 10.4271/2000-01-2315
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Design and Development of Loop Heat Pipes

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Cited by 8 publications
(5 citation statements)
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“…The constrained space of such applications requires to design specific LHPs. Various models have been developed for the LHP characterization [7,23,[29][30][31][32]. The steady state models are useful to size new-designed LHPs and to predict LHP performance for various fixed external conditions.…”
Section: Introductionmentioning
confidence: 99%
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“…The constrained space of such applications requires to design specific LHPs. Various models have been developed for the LHP characterization [7,23,[29][30][31][32]. The steady state models are useful to size new-designed LHPs and to predict LHP performance for various fixed external conditions.…”
Section: Introductionmentioning
confidence: 99%
“…The LHP was developed and tested in 1972 in the former Soviet Union [1]. The development of LHPs was a response to the challenge of the increasing needs of electronic systems, and with the specific demand of aerospace technology, which requires high operational reliability and robustness [2][3][4][5][6][7][8][9][10]. The two-phase loops offer many advantages over heat pipes [1,11] in terms of operation against gravity, maximum heat transport capability, smoothwalled flexible transport lines, and fast diode action.…”
Section: Introductionmentioning
confidence: 99%
“…Concerning the development of the LHP transient modeling, only a limited amount of publications exist in the open literature. Mena et al [10] have developed a transient model based on the energy and mass balance equations in a monodimensional hydraulic network. The mass flow rate was assumed to be constant at each instant in the whole loop and the pressure energy was neglected.…”
mentioning
confidence: 99%
“…The mass flow rate was assumed to be constant at each instant in the whole loop and the pressure energy was neglected. By comparing the calculation and experimental results, Mena et al [10] concluded that this modeling approach did not allow one to perform very accurate thermohydraulic analysis at the LHP level during the transient changes. Wrenn et al [11] have used the NASA-standard thermohydraulic analyzer, SINDA/FLUINT, which solves the conservation equations of mass, momentum, and energy.…”
mentioning
confidence: 99%
“…The purpose of this study was to develop a low-cost high-performance small LHP with a plastic wick for space and terrestrial applications. So far, there have been several reports on LHPs with plastic wicks [4][5][6][7][8]. However, detailed discussion of the properties and the advantages and disadvantages of plastic porous wicks have not been well discussed.…”
mentioning
confidence: 99%