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Ultramet
DUNS: 052405867
# of Employees: 67
HUBZone Owned: N
Socially and Economically Disadvantaged: N
Woman Owned: N
Award Charts
Award Listing
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Design, Fabrication, and Testing of a High Temperature Foam Core Heat Exchanger for Small Modular Reactors
Amount: $206,500.00A helium-cooled small modular reactor (SMR) can take advantage of the Brayton power conversion cycle with greater efficiency compared to the steam Rankine cycle. Alternatively, a more advanced supercr ...
SBIRPhase I2020Department of Energy -
Compact Heat Exchangers for Space Power Systems
Amount: $124,999.00For missions to dark, dusty, or distant destinations, solar power is not practical. General-purpose heat sources used in conjunction with a heat engine represent a viable solution. The critical challe ...
SBIRPhase I2020National Aeronautics and Space Administration -
Advanced Horizontal CVD Reactor Development for Increased Process Efficiency to Produce Seamless Thick-Film CVD Niobium-Lined Copper SRF Cavities
Amount: $206,500.00DOE is interested in innovative fabrication technologies for cost-effective high-Q, high-field superconducting radio frequency (SRF) cavities necessary for the economic viability of future accelerator ...
SBIRPhase I2019Department of Energy -
Integration of TRISO Fuel Particles with Open-Cell Foam for Increased Safety, Heat Transfer, and Fuel Performance
Amount: $206,500.00Tristructural isotropic (TRISO) fuel is a key component of advanced small modular nuclear fission reactors due to its inherent safety at high temperatures and irradiation levels and decreased prolifer ...
STTRPhase I2019Department of Energy -
Coatings for Protection against Hot Hydrogen in Solar-Thermal Propulsion
Amount: $125,000.00Advanced carbon-based heat exchangers (carbon/carbon composite or graphite) used in solar-thermal propulsion engines must be protected for extended periods from the ge;3000 K hydrogen propellant. In p ...
SBIRPhase I2019National Aeronautics and Space Administration -
Design and Fabrication of a Mars Ascent Vehicle Reaction Control System
Amount: $125,000.00Sample return missions generally have the largest velocity change (Delta;V) requirements for a mission to a given body such as Mars. For every pound of Mars liftoff mass removed from the return vehicl ...
SBIRPhase I2019National Aeronautics and Space Administration -
Combustion Chambers for Use with AF-M315E Monopropellant
Amount: $75,000.00The use of AF-M315E, a non-toxic monopropellant developed by the Air Force, promises substantial performance improvement and reduced cost compared with legacy hydrazine-based systems. Before the techn ...
SBIRPhase I2019Department of Defense Air Force -
Characterization and Scaleup of High Temperature Oxidation-Resistant Coatings for Carbon/Carbon Composites
Amount: $143,703.00Hypersonic flight performance of a lifting body vehicle design is improved significantly by the drag reduction achieved when nose and wing leading edges are sharp and shape-stable under all flight con ...
SBIRPhase I2019Department of Defense Air Force -
Low-Density Ablator-Filled Foam Incorporating Lyocell-Derived Carbon Fiber for BMDS Interceptors, Phase II
Amount: $996,716.00In previous exit cone insulator development for MDA and heat shield fabrication for NASA, Ultramet developed advanced foam-reinforced carbon/phenolic ablators, now at TRL 6, that offer substantially i ...
SBIRPhase II2018Department of Defense Missile Defense Agency -
CVD Process Development of Thin Film Triniobium-Tin on Copper SRF Cavities
Amount: $999,998.00Innovative fabrication technologies for cost-effective high-Q, high-field superconducting radio frequency (SRF) components are needed for the economic viability of future accelerator facilities. The w ...
SBIRPhase II2018Department of Energy
