SBIR/STTR Research Award

Pulsating Heat Pipes

Award identifier d64b6a3a3c170a74ee29773a92dfc05efeeb287215493be97d7740298bbbdfddAwarding agency National Aeronautics and Space Administration

Award amount

$124,731

Program and phase

SBIR · Phase I

Award year

2015

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Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
Peregrine Falcon Corporation
Proposal award date
2015-06-17
Contract end date
2015-12-17
UEI
LXQQB47E1RA3
Solicitation number
Not reported
Topic code
H8.01

Research abstract

An advanced heat transport technology is presented that can enable space nuclear power systems to transfer reactor heat, convert heat into electricity, reject waste heat, and provide high thermal conductivity to enhance waste heat transfer and radiator performance. This is a low cost, autonomous, high reliability and long-life solution. This technology can operate at high temperatures up to 1,000 K to either provide heat transport for reactor cooling or to dramatically increase thermal conductivity to provide the waste heat transfer for heat rejection systems. This innovative technology is based upon Peregrine's proprietary technology in pulsating heat pipes. Pulsating heat pipes are autonomous thermal transport systems that operate by pulsating action initiated by the introduction of heat and the extraction of heat to make a self-contained thermal transport device. This innovation will enable NASA missions to be more successful, more durable and of higher reliability, while also being very cost effective, lightweight and highly efficient. This innovation relies upon pulsating heat pipe technology where serpentine micro-channels are embedded within the plane of a sheet or plate of material. The micro-channels are partially charged with a working fluid. When heat is introduced to the PHP solid state device, vapor pressure locally increases (due to the serpentine pattern resistance) and vapor bubbles are created until the local increased pressure pulses from this high pressure area. At another area on this PHP device is the condenser (for thermal dissipation). In this area, heat is removed and vapor pressure is reduced, shrinking or contracting the bubbles. The pulsing from the evaporator and the contraction at the condenser, along with the system perturbations due to fluid contact angles and resistance within the serpentine channels, produces an autonomous, self-contained two-phase cooling system, in essence, the transfer of heat due to pressure changes.

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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