SBIR/STTR Research Award

Titanium-Water Heat Pipe Radiator for Spacecraft Fission Power

Award identifier 4254b4e64025226d8d95ea282c33ead47f17b98ede38b7673bcd56a15ad403a6Awarding agency National Aeronautics and Space Administration

Award amount

$124,902

Program and phase

SBIR · Phase I

Award year

2014

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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
2014-06-20
Contract end date
2014-12-19
UEI
Z8KVZV3DR7J4
Solicitation number
Not reported
Topic code
H8.02

Research abstract

The proposed program will develop titanium/water heat pipes suitable for Spacecraft Fission Power. NASA is examining small fission power reactors for future space applications with the most recent being Kilopower, which provides roughly 1 kW of electric power. Kilopower uses titanium/water heat pipes to remove the waste heat from the cold end of the convertors. Previous water heat pipe designs for space fission power are not suitable for Kilopower as they are either for surface fission power and use thermosyphons, or are grooved heat pipe designs, which are not suitable for ground testing. ACT will develop heat pipes with two different designs that are suitable for Kilopower: Hybrid grooved/screen wick and Self-venting arterial wick. Hybrid wick heat pipes will satisfy the Kilopower requirements and ACT has already successfully tested similar hybrid wick heat pipes. The self-venting arterial wick has not previously been tested in a vertical orientation but will be investigated as a higher performance, lower mass alternative to hybrid grooved pipes. The overall technical objective of the Phase I and Phase II projects is to develop a titanium/water heat pipe radiator suitable for Spacecraft Fission Power, such as Kilopower. During Phase I, ACT will investigate both a hybrid wick system, utilizing a screened evaporator and grooved condenser design, and a self-venting arterial wick design. The heat pipe design will also include a small NCG charge, which allows the fluid in the heat pipe to freeze in a controlled fashion as the heat pipe is shut down, avoiding damage, and aids with start-up from a frozen condition. In addition to testing the heat pipes in different orientations, freeze/thaw tolerance will also be demonstrated.

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.

Awards with the same topic code

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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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