SBIR/STTR Research Award

Consolidation of Heat Pipes within a U-8Mo Core for High Efficiency and Long-Term Reliability

Award identifier c64930178892038560e13449cb084db1a76bbe912b2cda4b19005e41ef36a769Awarding agency National Aeronautics and Space Administration

Award amount

$3,588,755

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
Peregrine Falcon Corporation
Proposal award date
2020-12-22
Contract end date
2022-12-21
UEI
LXQQB47E1RA3
Solicitation number
SBIR_20_P2S
Topic code
H8

Research abstract

A key requirement for high efficiency and the long-term reliability of Fission Power Systems (FPS) is the embedment and metallurgical connection of the heat pipes within the radioactive core material. Creating intimate contact between the heat pipes and the core material with a high thermal conductivity joint enables FPSs to operate at their optimum performance. This proposed Phase II Sequential Effort will advance NASArsquo;s Moon to Mars objectives by facilitating the rapid infusion of this consolidation and joining technology into NASArsquo;s FPSs, particularly for manned lunar missions by improving and optimizing the exchange of thermal energy at the heat pipe to the core interface. This Sequential effort is timely for infusion into upcoming designs for lunar missions; and that success then will be leveraged for Mars missions.nbsp;Peregrine Falcon Corporation (Peregrine) utilizing our proprietary technology in Liquid Interface Diffusion (LID) bonding will create a solid state joint between the Heat Pipe Wall material and the uranium core material of FPSs. LID bonding relies upon pressure and time at elevated temperatures to depress the melt point of an intermediate material to create incipient melting to initiate metallurgical joining. In this development, force is used to consolidate the heat pipe/core assembly to drive out any gaps and/or voids within the contained assembly and just as important develops pressure across the heat pipe to core interface.nbsp; Temperatures, durations and pressures have been selected and verified in Phase I and II to create a solid state joint resulting in a high thermal conductivity connection at the heat pipe to core interface. This allows FPSs to operate at their peak performance.nbsp;nbsp; nbsp;

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

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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