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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.
Federico R. Casci, Ettore Minardi
Fusion Science and Technology | Volume 4 | Number 1 | July 1983 | Pages 170-175
Technical Paper | Magnet System | doi.org/10.13182/FST83-A22783
Articles are hosted by Taylor and Francis Online.
The basic parameters characterizing the burn control with the vertical field in an ignited tokamak are discussed in a zero-dimensional model assuming a single circuit for the vertical field and neglecting passive effects. The behavior of the system is determined by three dimensionless quantities: ξ which includes the effect of the mutual inductance; Ũ , related to the gain of the linear feedback; and A, related to the pressure, to the plasma current, and to the vertical field index. Analysis of the circuit equations and of the transport equation leads to the determination of stability regions in the parameter space. It is shown that the effect of the mutual inductance described by ξ is always relevant in the choice of the parameters for a stable burn. As a practical illustration the results are applied to the INTOR case.