SBIR/STTR Research Award

Cryogenic Loop Heat Pipe

Award identifier 878e65cc31393ebf334bd688777c091980f0846adafb96af9056c1f7ce7b16d1Awarding agency National Aeronautics and Space Administration

Award amount

$69,978

Program and phase

SBIR · Phase I

Award year

1994

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Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
DYNATHERM CORP.
Proposal award date
Not reported
Contract end date
Not reported
UEI
Not reported
Solicitation number
Not reported
Topic code
Not reported

Research abstract

Cryogenic heat pipes are typically characterized by their low heat transport capability, resulting from the low surface tension and the low latent heat of their working fluids. These heat transfer limits restrict the amount of heat which can be removed from the device being cooled and/or the allowable separation between the heat source and the sink. Loop Heat Pipes offer significant improvements in heat transport over conventional heat pipes, due to their fine-pored wick structures and liquid and vapor transport lines which are optimized to minimize pressure drop. Loop Heat Pipes have demonstrated their performance advantages at ambient temperature, and have proven to be self-priming, reliable heat transfer devices. The primary goal of the proposed program is to extend this technology to cryogenic temperatures while maintaining the reliability of the ambient temperature devices. A prototype Loop Heat Pipe will be developed in Phase I, with the design goal of improving heat transport capability over state-of- the-art cryogenic heat pipes by an order of magnitude or more. Demonstration tests will characterize the prototype's steady state performance capabilities, as well as its startup behavior. The test results will also be used to validate/update existing analytical models.

Technology keywords

Not reported

Agency intelligence

National Aeronautics and Space Administration

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