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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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ANS Student Conference 2025
April 3–5, 2025
Albuquerque, NM|The University of New Mexico
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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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Fusion Science and Technology
Latest News
First astatine-labeled compound shipped in the U.S.
The Department of Energy’s National Isotope Development Center (NIDC) on March 31 announced the successful long-distance shipment in the United States of a biologically active compound labeled with the medical radioisotope astatine-211 (At-211). Because previous shipments have included only the “bare” isotope, the NIDC has described the development as “unleashing medical innovation.”
Yasunori Iwai, Katsumi Sato, Toshihiko Yamanishi
Fusion Science and Technology | Volume 66 | Number 1 | July-August 2014 | Pages 214-220
Technical Paper | doi.org/10.13182/FST13-725
Articles are hosted by Taylor and Francis Online.
We have developed a honeycomb palladium catalyst to be used for the oxidation of tritiated hydrocarbons. Since the suitable loading rate of palladium deposited on the base material is a technical point, honeycomb-shaped palladium catalysts of three different loading rates—2, 5, and 10 g/L—were prepared to investigate the effect of loading rate of palladium on reaction rate in this study. Tritiated methane was selected as the typical hydrocarbon. A 12 m3 tank was prepared to prevent tritiated methane at tracer concentration fed to the catalytic reactor from fluctuating. The overall reaction rate constant for tritiated methane oxidation on the honeycomb palladium catalyst was determined with a flow-through system as a function of space velocity from 1000 to 6300 h−1, methane concentration in carrier from 0.004 to 100 ppm, and temperature of catalyst from 322 to 673 K. The honeycomb palladium catalyst without pretreatment for activation initially lowers the overall reaction rate constant at lower temperatures. However, the constant recovers steeply to the original value during the continuous combustion of tritiated methane. The loading rate of palladium deposited on the base material has little effect on reaction rate for tritiated methane combustion. The overall reaction rate constant is proportional to the space velocity. The overall reaction rate constant is independent on the methane concentration when it is less than 10 ppm.
