SBIR/STTR Research Award

(U,Zr)C Mixed Carbide Fuel Coatings Using Impulse PVD

Award identifier a56a262c812ae4ee2e2ed76eda7c7617a11b122c8b50f35d5e90e88eeedf16a2Awarding agency National Aeronautics and Space Administration

Award amount

$125,000

Program and phase

SBIR · Phase I

Award year

2020

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Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
STARFIRE INDUSTRIES, LLC
Proposal award date
2020-08-12
Contract end date
2021-03-01
UEI
GZ2MY2S55JW9
Solicitation number
SBIR_20_P1
Topic code
Z10

Research abstract

NTP hasnbsp;multiple goals ranging from higher exhaust temperature (gt;1000s Isp), hot corrosion resistance (diverse propellants: H2, CH4, NH3, H2O), higher power density (thrust, gt;5MW/L goal), local fission product retention (materials damage, migration), manufacturability (cost, materials), safety (ground testing, flight), long core lifetime for interplanetary round trips (single fuel load, good burnup, control, 5+ years), and commonality with terrestrial applications (SMR, MNR, industrial heat, DoD/Pele) and advanced applications like reusable hypersonics, Luna/Mars surface power).nbsp;A solution, called the Coated Mixed Carbide (CMC) fuel element approach, is a hybrid between distributed solid-solution carbides from the Rover/NERVA days and localized TRISO fuel from todayrsquo;s small modular reactor concepts.nbsp; Very high temperature ~3500Knbsp;(U,Zr)C fuel is concentrated in small kernels and protected against attack bynbsp;hydrogen from outsidenbsp;and from fission products within by engineered multilayered coatings.nbsp; An recent innovationnbsp;in high-powernbsp;impulse magnetron sputtering (i.e.nbsp;IMPULSEreg; + Positive Kicktrade;) allows conformalnbsp;coatings of thenbsp;small-diameter fuel kernels with lsquo;TRIZO-likersquo; protective layers to enable high-power density NTP reactors.nbsp; With precision ion energy and deposition flux control, each multilayer can be engineered for specific property, such as fission gas retention, compressive stress, hydrogen permeability, ductility, etc.nbsp;These #39;TRIZO-like#39; pellets are embedded in a ZrC(W) matrix and distributed for lower peaking factor across the fuel element.nbsp; Embedded propellant channels can be used for direct nuclear thermal propulsion or bimodal heat pipe power extraction for electrical power generation.This Phase I SBIR builds on three patent-pending technologies and seeks to demonstrate feasibility of the concept, identity and rank technical risks and prioritize investment in Phase II towards retiring the necessary risks.

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

61 SBIR/STTR records share this UEI (2003–2025). Reported award amounts total $32,483,674. Reported amounts are not federal obligations.

Phases: Phase I, Phase II, Phase II – Direct to Phase II

Agencies: Department of Energy, Department of Defense, National Science Foundation, National Aeronautics and Space Administration, Department of Homeland Security

Agency intelligence

National Aeronautics and Space Administration

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