SBIR/STTR Research Award

Refractory Open-Cell Foam Fuel for High-Efficiency Nuclear Space Propulsion, Phase II

Award identifier 871bf2a354dc90f0e3e61690c83c5fc30573f8c4857ccbbfa523cdaaec71746cAwarding agency National Aeronautics and Space Administration

Award amount

$500,000

Program and phase

STTR · Phase II

Award year

2004

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Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
ULTRAMET
Proposal award date
Not reported
Contract end date
Not reported
UEI
N8ZRMWX85NZ6
Solicitation number
Not reported
Topic code
Not reported

Research abstract

Low-density, high specific stiffness ceramic and metal open-cell foams may be utilized for creation of an innovative fuel element for use in space nuclear reactors. Highly porous structural foam may be developed for high thermal efficiency, high temperature fuel elements for both propulsion and gas-cooled power reactors. Current designs, such as annular rods or pebble beds, cannot operate at extremely high temperatures and thus limit efficiency. In the proposed Phase II project, the foam fuel element material will consist of a tricarbide, U(ZrNbC), composed of uranium carbide that is vapor infiltrated into a foam matrix of niobium carbide and zirconium carbide (in Phase I, tantalum carbide was substituted for uranium carbide). The porous foam structure provides an extended surface area for highly efficient heat transfer and reduces density, reducing hydrogen turbopump power demands and increasing thrust-to-weight ratio. In Phase I, Ultramet teamed with Sandia National Laboratories to demonstrate the feasibility of these highly innovative foam fuel elements. This work included chemical vapor infiltration of the carbides into an open-cell foam skeletal structure by Ultramet and fabrication of a matrix of foam densities for thermal/gas flow testing at Sandia. The results of flow testing, coupled with the results of thermomechanical modeling performed at Sandia, confirmed the high potential of this design following continued development. In Phase II, Ultramet and Sandia propose to develop and demonstrate fabrication of the actual (U-Zr-Nb)C foam fuel material. Ultramet will finalize process optimization using the (Ta-Zr-Nb)C material and provide the processing conditions to Sandia which, in conjunction with the University of Florida Institute of Space Power and Propulsion (INSPI) facility, will produce and test (U-Zr-Nb)C foam in a hot hydrogen environment. Sandia will also perform comprehensive thermomechanical modeling, expanding on the modeling performed in Phase I.

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

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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