SBIR/STTR Research Award

3D Printed Loop Heat Pipe

Award identifier d00459d8fc3fd0356dcef8a7e3fdf1b610dc72402e9194577a384b84af4b4ab3Awarding agency National Aeronautics and Space Administration

Award amount

$749,857

Program and phase

SBIR · Phase II

Award year

2021

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Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
ADVANCED COOLING TECHNOLOGIES INC
Proposal award date
2021-08-09
Contract end date
2023-08-08
UEI
Z8KVZV3DR7J4
Solicitation number
SBIR_20_P2
Topic code
S3

Research abstract

The fast-growing space industry results in increasing demand for thermal control systems.nbsp; Loop heat pipes (LHPs) are a commonly utilized device for spacecraft due to high efficiency and flexibility (ability to integrate with deployable radiator, thermal control valve, etc.).nbsp; However, they are currently too costly to manufacture to make them viable for most cost-sensitive applications such as CubeSats and SmallSats.nbsp; Conventional loop heat pipe manufacturing method involves multiple labor-intensive steps including a knife edge seal process to ensure no back leak of vapor that affects the thermal transport capability.nbsp; Unfortunately, the steps to manufacture the wick, insert it in the LHP evaporator, and seal with a knife edge results in very high manufacturing costs.nbsp; Advanced Cooling Technologies, Inc. (ACT) has developed a low-cost LHP evaporator using a technique called Direct Metal Laser Sintering (DMLS), otherwise known as 3D printing.nbsp; With the capability of building a porous wick structure together with a solid wall via additive manufacturing, 3D printed LHP eliminates the knife edge seal as well as many wick manufacturing and testing steps.nbsp; The 3D printed LHP reduces the fabrication cost by an order of magnitude, which enables the use of LHPs in many emerging space applications, including CubeSats and SmallSats.nbsp;While the developed 3D printed loop heat pipe shows significant cost benefit compared to the loop heat pipe made by conventional fabrication process, the pore size of 3D printed primary is around 5~7 mu;m, much larger than the 1 mu;m pore size made by sintering process.nbsp; In addition, the porosity of the 3D printed primary wick is lower than sintering wick (31% vs. gt; 40%).nbsp; In order to apply this emerging technology to higher power, large satellite applications, which are the current main loop heat pipe market, further reduce pore size and increase porosity are needed.

Technology keywords

Not reported

Other awards by this recipient

Verified by the same UEI. These are other public SBIR/STTR award pages, not a merged company record.

Research funding history

282 SBIR/STTR records share this UEI (2003–2026). Reported award amounts total $118,415,811. Reported amounts are not federal obligations.

Phases: Phase I, Phase II, Phase II – Direct to Phase II

Agencies: Department of Defense, National Aeronautics and Space Administration, Department of Energy, National Science Foundation, Department of Agriculture, Department of Health and Human Services

Agency intelligence

National Aeronautics and Space Administration

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