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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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2024 ANS Annual Conference
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Proving DRACO will deliver
The United States is now closer than it has been in over five decades to launching the first nuclear thermal rocket into space, thanks to DRACO—the Demonstration Rocket for Agile Cislunar Orbit.
M. Ulrickson, G. Barnes, H.M. Fan, G. Labik, D. Loesser, L. Lontai, D.K. Owens
Fusion Science and Technology | Volume 21 | Number 3 | May 1992 | Pages 1817-1822
Plasma-Facing Component | doi.org/10.13182/FST92-A29982
Articles are hosted by Taylor and Francis Online.
Carbon fiber composite (CFC) materials have been used as the plasma facing surface on limiters in TFTR since 1989. We changed from all POCO graphite tiles on the inner bumper limiter (BL) to about 1/3 CFC tiles in the high heat flux area because of tile failures with heating powers up to 20 MW. The RF limiters (RFL), which were designed to protect the radio-frequency antennas from plasma heat flux, were designed with CFC material. This paper discusses the design issues related to the CFC materials, our experience with material property variations in large production runs, and our operational experience with CFC limiters. The replacement BL tiles were made from a 3D CFC material. The RFL tiles were made from a 2D CFC. The use of 2D CFC material was molded to near net shape. The tiles were required to withstand up to 105 cycles of 50 MW of heating power for a duration of 2 s. Determination of the minimum material properties was one of the major design issues. The fabrication of the BL tiles required production of about 35 large billets of 3D CFC material. The fabrication of the RFL tiles required production of about 160 tile blanks. We found substantial variation in the material properties of the finished parts. The distribution of the material property data is discussed. In the case of the RFL tiles some parts did not meet the required properties because of the non-standard nature of the fabrication. After nearly two years of operation on the CFC tiles, none of the CFC tiles have failed. The only damage observed on the CFC tiles is a slight darkening of the tile when it is heated to the sublimation point by the disruption heat loads. Recommendations of the best design and fabrication strategies for CFC plasma facing components are made.