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A year in orbit: ISS deployment tests radiation detectors for future space missions
The predawn darkness on a cool Florida night was shattered by the ignition of nine Merlin engines on a SpaceX Falcon 9 rocket. The thrust of the engines shook the ground miles away. From a distance, the rocket appeared to slowly rise above the horizon. For the cargo onboard, the launch was anything but gentle, as the ignition of liquid oxygen generated more than 1.5 million pounds of force. After the rocket had been out of sight for several minutes, the booster dramatically returned to Earth with several sonic booms in a captivating show of engineering designed to make space travel less expensive and more sustainable.
Xiaole Wang, Leisheng Chen, Ruixiang Sun, Jaeyoung Lee
Nuclear Technology | Volume 211 | Number 8 | August 2025 | Pages 1662-1673
Research Article | doi.org/10.1080/00295450.2024.2425915
Articles are hosted by Taylor and Francis Online.
Inserting small spheres of a fixed size into a pebble bed can enhance heat transfer, lower the surface temperature of fuel elements, and reduce the risk of local hot spots. However, does a multisized pebble bed outperform a double-sized pebble bed in terms of heat transfer? To address this question, numerical simulations were conducted to evaluate the heat transfer characteristics of face-centered-cubic-structured pebble beds with two and three types of small spheres, maintaining a constant solid volume. The results showed that the average heat transfer coefficients of the multisized pebble bed were nearly identical to those of the double-sized bed. This suggests that using two types of small spheres does not necessarily provide better heat transfer performance than using a double-sized bed. Additionally, the number, size, and placement of the spheres influenced the pressure drop. These findings offer insights into the heat transfer behavior of high-temperature reactor cores and provide a useful reference for the design of future pebble bed reactor cores.