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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.
Richard P. Burke, Peter W. Huber
Nuclear Technology | Volume 49 | Number 3 | August 1980 | Pages 374-379
Technical Paper | Reactor | doi.org/10.13182/NT80-A17685
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Predictions from a one-dimensional pool swell model are compared with results from small-scale pool swell tests. The main elements of the model other than the geometric simplification are identical to the assumptions that underlie the hydrodynamic scaling laws investigated in the pool swell experiments. The favorable comparison between prediction and experiment demonstrates that all key features of the data can be explained qualitatively and are quantitatively within physically reasonable ranges. An experimental record of air bubble growth history is compared with the predictions from an axisymmetric pool swell code calculation.