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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
June 16–19, 2024
Las Vegas, NV|Mandalay Bay Resort and Casino
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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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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.
R.L. Engelstad, J.W. Powers, E.G. Lovell
Fusion Science and Technology | Volume 19 | Number 3 | May 1991 | Pages 697-702
Inertial Fusion | doi.org/10.13182/FST91-A29426
Articles are hosted by Taylor and Francis Online.
Results are presented for the preliminary mechanical design of a light ion beam Laboratory Microfusion Facility (LMF). Applications of the facility include the development of high gain, high yield ICF targets. The LMF target chamber must meet the requirements imposed by the ion beam propagation, and survive severe target blast loadings. Yields from 10 to 1000 MJ are considered for a projected lifetime of up to 15,000 shots. The chamber will be subjected to repeated loadings that include intense x-ray vaporization of the first wall surface, resulting in large amplitude pressure waves. A carbon/carbon composite thermal liner has been proposed to attenuate the radial shock waves and protect the structural wall. Nevertheless, the chamber wall must still be designed to withstand large impulsive and residual pressures. The proposed target chamber consists of a capped cylindrical shell that is 1.5 m in radius and 4.5 m in height. The analysis of the mechanical response of the structural wall from the repetitive dynamic overpressures is described in detail. Modified elastic constants are used to account for the higher ligament stresses and strains which are present between the beam ports and diagnostic ports. In addition, fatigue lifetime calculations have been made according to ASME guidelines, applying cumulative damage criteria specified by Miner's rule. A modified rainflow cycle counting method was used in conjunction with Goodman diagrams to determine equivalent stresses and strains to be used with the constant amplitude, fully reversed fatigue data. Both 6061-T6 aluminum and 2 1/4 Cr - 1 Mo steel are considered for the structural materials, with maximum stress and fatigue design results developed for a range of thicknesses and overpressures.