Refractory Open-Cell Foam Fuel Matrix for High-Efficiency Nuclear Space Propulsion Systems

Award Information
Agency:
National Aeronautics and Space Administration
Branch
n/a
Amount:
$100,000.00
Award Year:
2003
Program:
STTR
Phase:
Phase I
Contract:
NAS8-03038
Award Id:
61923
Agency Tracking Number:
020014
Solicitation Year:
n/a
Solicitation Topic Code:
n/a
Solicitation Number:
n/a
Small Business Information
12173 Montague St, Pacoima, CA, 91331
Hubzone Owned:
N
Minority Owned:
N
Woman Owned:
N
Duns:
n/a
Principal Investigator:
Brian Williams
() -
brian.williams@ultramet.com
Business Contact:
Craig Ward
Engineering Administrative Mgr
(818) 899-0236
craig.ward@ultramet.com
Research Institution:
Sandia National Laboratories
Dennis Youchison
P.O. Box 5800
Albuquerque, NM, 87185
(505) 845-3138
Nonprofit college or university
Abstract
Low-density, high specific stiffness ceramic and metal open-cell foam materials may be utilized for creation of an innovative fuel matrix 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 this project, the foam fuel material will ultimately consist of a tricarbide, UZrNbC, composed of enriched uranium that is vapor infiltrated into a foam matrix of niobium carbide (NbC) and zirconium carbide (ZrC), although tantalum carbide (TaC) will be substituted for uranium carbide (UC) during initial development. The porous 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. The foam matrix can have 80-90% open porosity for maximum convection, and the ligament dimensions can be tailored to provide either good or poor thermal conduction as needed. Recent work on porous materials has demonstrated effective heat transfer coefficients with helium near 26,000 W/m2?K. NbC and ZrC foams have several important advantages over other high temperature materials, including low density, lack of degradation in hydrogen at 3000 K (where they also retain structural integrity), and minimal neutron cross-section. The dispersed fissile material is an integral part of a high-conductivity matrix. Thus, a much lower temperature difference can exist between the fuel and the propellant. Extremely high outlet temperatures can be achieved, yielding the high specific impulse required for interplanetary exploration. Ultramet will team with Sandia National Laboratories to demonstrate the feasibility of integrating porous foam fuel elements into a new reactor concept for compact, high-performance space reactors.

* information listed above is at the time of submission.

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