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DOE selects first companies for nuclear launch pad
The Department of Energy’s Office of Nuclear Energy and the National Reactor Innovation Center have announced their first selections for the Nuclear Energy Launch Pad: three companies developing microreactors and one developing fuel supply.
The four companies—Deployable Energy, General Matter, NuCube Energy, and Radiant Industries—were selected from the initial pool of Reactor Pilot Program and Fuel Line Pilot Program applicants, the two precursor programs to the launch pad.
W. Breitung, S. A. Wright
Nuclear Science and Engineering | Volume 105 | Number 4 | August 1990 | Pages 303-318
Technical Paper | doi.org/10.13182/NSE90-A21467
Articles are hosted by Taylor and Francis Online.
Irradiated (U.Pu)-mixed oxide with 5% burnup was heated in the pulsed Annular Core Research Reactor at Sandia National Laboratories. The tests were typical of prompt Bethe-Tait excursions in terms of heating method (nuclear fission), heating period (milliseconds), and temperatures attained (up to 7700 K). Fission products provided high pressures at temperatures at which fresh fuel shows only a negligible vapor pressure. Fission product release became measurable as soon as the temperature exceeded the steady-state irradiation temperature of the fuel sample. The fission product pressures reached 1.3 to 2.5 MPa at 3000 K over solid fuel, and 2.5 to 5 MPa at 4000 K over liquid fuel. The total amount of fission product released corresponded to ∼30 to 75% of the fission gas inventory. The amount of fission product released increased with the fuel heating rate. Under rapid heating, the total pressure over irradiated (U,Pu) oxide is controlled by a suppression mechanism. At any given temperature, the gaseous components (xenon, cesium, and ambient gas) suppress fuel boiling if their pressure pgas is higher than the fresh fuel saturation vapor pressure psat of unirradiated fuel. If psat exceeds pgas, the total pressure is, to a first approximation, equal to Psat. Under millisecond heating, the total pressure from irradiated fuel may be taken as ptot = max(Pgas,Psat).