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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.
Meeting Spotlight
Conference on Nuclear Training and Education: A Biennial International Forum (CONTE 2025)
February 3–6, 2025
Amelia Island, FL|Omni Amelia Island Resort
Standards Program
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
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Christmas Night
Twas the night before Christmas when all through the houseNo electrons were flowing through even my mouse.
All devices were plugged in by the chimney with careWith the hope that St. Nikola Tesla would share.
M. Z. Hasan, T. Kunugi, M. Seki, M. Yokokawa, H. Ise, H. Kaburaki, The ARIES team
Fusion Science and Technology | Volume 19 | Number 3 | May 1991 | Pages 908-912
Advanced Reactor | doi.org/10.13182/FST91-A29460
Articles are hosted by Taylor and Francis Online.
The response of ARIES-I divertor plate to hard plasma disruptions has been analyzed numerically by a two-dimensional transient heat transfer code. For ARIES-I, the estimated thermal quench time is 0.3 msec and the average heat flux is 8.8×109 W/m2 with a peaking factor of 5. The divertor plate is made of 2.5 mm diameter SiC tubes with wall thickness of 0.5 mm and coated with a 2 mm layer of tungsten on the plasma facing side. The analysis predicts a total material erosion per disruption of about 111 µm without vapor shield and 48 µm with a simple vapor-shield model. The designated 1 mm of the tungsten coating for disruption is expected to last about 20 disruptions. A two-dimensional thermo-fluid dynamic analysis of the melt layer under the influence of buoyancy and surface tension forces has been performed. The results tend to imply that the melt layer is relatively unaffected during the disruption, especially for short thermal quench time.