SBIR/STTR Research Award

Pulsating Heat Pipes

Award identifier 5b2d2638f894726733b4d76cee24e3b71d282b01d1d37906c66db07bc890f347Awarding agency National Aeronautics and Space Administration

Award amount

$747,469

Program and phase

SBIR · Phase II

Award year

2016

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Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
Peregrine Falcon Corporation
Proposal award date
2016-04-28
Contract end date
2018-04-27
UEI
LXQQB47E1RA3
Solicitation number
Not reported
Topic code
H8.01

Research abstract

Large radiator panels, based upon state of the art conventional heat pipes with attached fins for thermal load distribution and dissipation is the current baseline design for NASA?s Fission Power System. The initial 1 kWe FPS requires a total radiating surface of 2.5 m2. Higher power designs will require corresponding larger radiating surfaces. In order to achieve optimum radiator performance, the face sheets of these radiators should present waste heat loads as isothermal sheets pointed to the sink of space. The current state of the art designs do not meet this requirement and rely upon heat pipes to axially carry the waste thermal loads while radiating fins, with typical thermal gradients and losses, provide thermal distribution away from the heat pipes via simple conduction. Under Phase I, Peregrine has successfully demonstrated an alternative design which promises to be lower in mass while improving performance based upon pulsating heat pipes (PHPs). PHPs can directly acquire and then readily distribute thermal loads across the face of radiator panels to create highly efficient near isothermal designs. PHPs are an autonomous, self-contained, low profile, lightweight, high performance thermal transport system based upon heat of vaporization. Phase II will characterize a titanium/water pulsating heat pipe system, build prototypes of a Pulsating Heat Pipe (PHP) radiator for a 1 kWe FPS, and also build a conventional heat pipe design in order to provide a side by side comparison of performance increases of PHPs versus the conventional design. Phase II will provide objective data through empirical results for future efficient lightweight, isothermal radiator designs.

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

Verified by an exact topic code match. This is not a text-similarity match.

Research funding history

40 SBIR/STTR records share this UEI (2006–2025). Reported award amounts total $21,699,551. 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

Agency intelligence

National Aeronautics and Space Administration

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