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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.
Lei Wu, Jianjun Wang, Zhongning Sun
Nuclear Technology | Volume 211 | Number 6 | June 2025 | Pages 1202-1217
Research Article | doi.org/10.1080/00295450.2024.2385217
Articles are hosted by Taylor and Francis Online.
Submerged steam jet condensation is widely applied in many industrial fields due to its high heat and mass transfer efficiency during the process of direct contact condensation (DCC). The injection of steam into a water pool usually passes through an array of nozzles. It is important to understand the interaction between neighboring jets from different nozzles.
In this paper, two thermal resistance models for DCC are implemented into the computational fluid dynamics code ANSYS Fluent through a user-defined function. The triple steam nozzle cases, in which the inlet pressure ranges from 0.1 to 0.6 MPa, were investigated to understand the interaction of nozzles and their configuration as well as their mechanisms. The distributions of temperature, velocity, volumetric fraction, and pressure fields were analyzed for different cases. Furthermore, the plumes of steam jets always attract each other toward the center of the plumes, and when the inlet pressure is over 0.3 MPa, the mixing of neighboring steam plumes will occur.
In addition, the location where the peak value occurs for the parameters of steam velocity, pressure, and temperature, etc. is getting closer and closer to the center of the flow domain. In addition, the curve of the pressure along the centerline of the nozzle verified the existence of compression and expansion of steam inside the plume.