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Fusion Science and Technology
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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.
G. Van Oost, V. P. Bhatnagar, T. Delvigne, P. Descamps, F. Durodié, R. Koch, A. M. Messiaen, D. I. C. Pearson, P. E. Vandenplas, A. Vanderstraeten, R. Van Nieuwenhove, G. Van Wassenhove, R. R. Weynants, W. Kohlhaas, C. Stickelmann, A. Cosler, B. Giesen, B. Goerg, S. Haltrich, P. Huettemann, M. Korten
Fusion Science and Technology | Volume 12 | Number 3 | November 1987 | Pages 449-475
Technical Paper | Plasma Heating System | doi.org/10.13182/FST87-A25078
Articles are hosted by Taylor and Francis Online.
A multimegajoule ion cyclotron resonance heating (ICRH) experiment was installed on the Torus Experiment for Technology-Oriented Research (TEXTOR) tokamak. The system consists of two independent power lines each designed to generate and launch 1.5 MW of radio-frequency (rf) power into the machine during a 3-s period in the 25- to 29-MHz frequency range. Each power line consists of the following items: (a) a 1.5-MW transmitter, (b) a transmission line system, including a two-stub tuner, made of pressurized 155.6-mm (6.125-in.) and 228.6-mm (9-in.) rigid coaxial line components, and (c) an interface linking the transmission line to the antenna of the shielded stripline type placed along the tokamak's hot liner. Details of the line and antenna diagnostics and data acquisition system together with the subsequent impedance characteristic calculations are given. The rf radiation shielding for the ICRH experiment is explained. The control of the rf setup as a TEXTOR subsystem and the generator pulse control and operation modes are outlined. The antenna loading and power limitation in the presence of plasma and the conditioning procedure are discussed. Finally, the new rf system compatible with the toroidal pump limiter Advanced Limiter Test-II is presented.