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Division Spotlight
Thermal Hydraulics
The division provides a forum for focused technical dialogue on thermal hydraulic technology in the nuclear industry. Specifically, this will include heat transfer and fluid mechanics involved in the utilization of nuclear energy. It is intended to attract the highest quality of theoretical and experimental work to ANS, including research on basic phenomena and application to nuclear system design.
Meeting Spotlight
2025 ANS Annual Conference
June 15–18, 2025
Chicago, IL|Chicago Marriott Downtown
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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Latest News
Canada clears Darlington to produce Lu-177 and Y-90
The Canadian Nuclear Safety Commission has amended Ontario Power Generation’s power reactor operating license for Darlington nuclear power plant to authorize the production of the medical radioisotopes lutetium-177 and yttrium-90.
George H. Miley et al.
Fusion Science and Technology | Volume 56 | Number 1 | July 2009 | Pages 533-539
Experimental Facilities and Nonelectric Applications | Eighteenth Topical Meeting on the Technology of Fusion Energy (Part 1) | doi.org/10.13182/FST09-A8958
Articles are hosted by Taylor and Francis Online.
Earlier studies have described Inertial Electrostatic Confinement (IEC) fusion power concepts using either D-He3 or p-B11 fuels to provide a high-power density fusion propulsion system capable of aggressive deep space missions. However, this requires a large multi-GW thruster forcing a long term development program. As a first step, we examine here a progression of near-term IEC thrusters, stating with a 1-10 kWe electrically-driven IEC jet thruster for satellites followed by a small 50-100 kW IEC fusion thruster module for next generation large deep space spacecraft. The initial electrically-powered unit is a novel multi-jet plasma thruster based on spherical IEC technology using electrical input power from a solar panel. This type of unit is discussed and its advantages for next step electrically driven units are identified.