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Conference Spotlight
2026 Annual Conference
May 31–June 3, 2026
Denver, CO|Sheraton Denver
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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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Modernizing I&C for operations and maintenance, one phase at a time
The two reactors at Dominion Energy’s Surry plant are among the oldest in the U.S. nuclear fleet. Yet when the plant celebrated its 50th anniversary in 2023, staff could raise a toast to the future. Surry was one of the first plants to file a subsequent license renewal (SLR) application, and in May 2021, it became official: the plant was licensed to operate for a full 80 years, extending its reactors’ lifespans into 2052 and 2053.
Shiyi He, Yan Xia, Fei Xu, Leidang Zhou, Xiaoping Ouyang
Nuclear Science and Engineering | Volume 195 | Number 2 | February 2021 | Pages 148-160
Technical Paper | doi.org/10.1080/00295639.2020.1794454
Articles are hosted by Taylor and Francis Online.
Alpha-decay propulsion technology, a microthrust technology based on thin spontaneous-alpha-decay films, is proposed in this paper. A large quantity of decayed alpha particles emitted from the upper surface of thin films would generate thrust statistically. Simulations were executed using the Monte Carlo N-Particle Transport Code (MCNP) to acquire the energy and angular distributions of escaping alpha particles, as well as the key parameters of alpha-decay films. A 22.40-μm 210Po film combined with a 20-μm aluminum film was able to generate an average thrust of 29.5 nN/cm2 in half-life time. The remaining charges and thermal energies of the decay films were considered. Directional-generated alpha particles were simulated to analyze the influence of angular scattering on escaped alpha-particle distributions. Alpha particles with low energy, with large scattering angles, or with large generated angles contributed less to thrust value. With the assumptions of no scattering, constant stopping power, and no range struggling, a set of analytic formulas were derived. Comparisons of the distributions and typical parameters between simulations and the analytic model were conducted. Discrepancies were mostly caused by the three assumptions and were less than 3.7% for thrust and less than 3.9% for the proportion of escaped alpha-particles.