SBIR/STTR Research Award

High-Emissivity CVD Dendritic Rhenium Coatings for NEP Radiator Panels, Phase II

Award identifier 67b815b7d97d6a30c605bd592a21f000276960bb21292eb82c254b911f200367Awarding agency National Aeronautics and Space Administration

Award amount

$850,000

Program and phase

SBIR · Phase II

Award year

2024

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Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
ULTRAMET
Proposal award date
2024-07-09
Contract end date
2026-07-08
UEI
N8ZRMWX85NZ6
Solicitation number
SBIR_23_P2
Topic code
Z10

Research abstract

Nuclear-electric propulsion (NEP) can significantly reduce mission durations for space exploration by providing substantially greater propulsion efficiency over chemical propulsion. NEP development is dependent on advances in several key technology areas, one of which is the primary heat rejection subsystem, which will account for a significant portion of the total spacecraft mass. Improved radiator panels, with lighter weight and higher emissivity, are needed, enabling reduced panel size for a reduction in the overall vehicle mass and more effective heat rejection for a more efficient propulsion system. The state-of-the-art space radiator material system uses carbon/carbon (C/C) or titanium panels with integrated titanium heat pipes. To increase radiator emissivity, Ultramet is depositing a thin, highly emissive dendritic rhenium coating on carbon and titanium with minimal effect on overall weight. In Phase I, coated coupons of representative carbon and titanium materials were sent to the University of Michigan for characterization and testing.nbsp;Coating survivability was demonstrated through exposure at various angles to ion bombardment from a Hall thruster ion plume, with microscopic imaging and emissivity measurements done before and after exposure. The dendritic microstructure and high emissivity of the rhenium coatings were unaffected after ion exposure in most cases. In Phase II, Ultramet will team with ThermAvant Technologies to demonstrate the increased heat rejection provided by the dendritic rhenium coating on additively manufactured titanium, diffusion-bonded titanium plate, and C/C subscale radiator panels with integrated titanium heat pipes. Coated subscale panels of each material will be fabricated and tested in relevant in-space operating conditions in a thermal vacuum chamber at NASA Glenn Research Center. A full-scale radiator panel design and manufacturing plan will be developed based on the results of the demonstration testing.

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

380 SBIR/STTR records share this UEI (1983–2025). Reported award amounts total $105,154,309. 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 Transportation, Department of Health and Human Services

Agency intelligence

National Aeronautics and Space Administration

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