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Aerospace Nuclear Science & Technology
Organized to promote the advancement of knowledge in the use of nuclear science and technologies in the aerospace application. Specialized nuclear-based technologies and applications are needed to advance the state-of-the-art in aerospace design, engineering and operations to explore planetary bodies in our solar system and beyond, plus enhance the safety of air travel, especially high speed air travel. Areas of interest will include but are not limited to the creation of nuclear-based power and propulsion systems, multifunctional materials to protect humans and electronic components from atmospheric, space, and nuclear power system radiation, human factor strategies for the safety and reliable operation of nuclear power and propulsion plants by non-specialized personnel and more.
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International Conference on Mathematics and Computational Methods Applied to Nuclear Science and Engineering (M&C 2025)
April 27–30, 2025
Denver, CO|The Westin Denver Downtown
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The Standards Committee is responsible for the development and maintenance of voluntary consensus standards that address the design, analysis, and operation of components, systems, and facilities related to the application of nuclear science and technology. Find out What’s New, check out the Standards Store, or Get Involved today!
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DTE Energy studying uprate at Fermi-2, considers Fermi-3’s prospects
DTE Energy, the owner of Fermi nuclear power plant in Michigan, is considering an extended uprate for Unit 2 that would increase its 1,100-MW generation capacity by 150 MW.
William E. Kastenberg, Paul L. Chambré
Nuclear Science and Engineering | Volume 31 | Number 1 | January 1968 | Pages 67-79
Technical Paper | doi.org/10.13182/NSE68-A18009
Articles are hosted by Taylor and Francis Online.
The spatial and temporal behavior of neutron distributions governed by the nonlinear diffusion equation approximation to neutron transport theory are considered in this paper. Stability criteria for the equilibrium states of various reactor feedback models are determined by the method of comparison functions. The comparison functions are used to construct simple solutions with error bounds to the equations considered. The two reactor models considered are the prompt feedback and the adiabatic model. The stability of the equilibrium state was found to be governed by the generalized buckling κ and its relationship to μ the lowest eigenvalue of the associated linear Helmholtz equation. Negative feedback is considered in both cases. Since the comparison functions bound the true solution from above and below, one can determine absolute errors of the approximations involved when constructing solutions. In a similar fashion, a bound on the maximum value of the excursion can also be obtained with little extra effort.