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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.
R. J. Hooper, S. S. Kalsi
Fusion Science and Technology | Volume 4 | Number 2 | September 1983 | Pages 1341-1345
Magnet Engineering | doi.org/10.13182/FST83-A23042
Articles are hosted by Taylor and Francis Online.
The design of resistive copper toroidal field (TF) coils is described for use in a nearterm tokamak fusion device (FED-R). A design requirement on the TF coils is that they contain readily demountable joints to facilitate replacement of components inside the bore of the coil. The coils are fabricated from rectangular window frame plates with 1-m-radius fillets in the inside corners. Each coil contains 17 turns — fabricated from CDA-110 copper plate segments 6.1 em thick. Because of high radiation fluence, a ceramic turn-to-turn insulator is used. The cooling system is sized to accommodate the combined heat loading that results from resistive power dissipation and nuclear heating.