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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.
J. D. Gordon, D. H. Berwald, B. A. Flanders, J. K. Garner, S. C. Mortenson, J. F. Parmer, C. A. Sink, J. C. Yu, K. L. Agarwal, S. Dharmarajn, N. M. Ghoniem, N. J. Hoffman, J. R. Bilton, B. E. Kirstein
Fusion Science and Technology | Volume 4 | Number 2 | September 1983 | Pages 1233-1238
Blanket and First Wall Engineering | doi.org/10.13182/FST83-A23026
Articles are hosted by Taylor and Francis Online.
A new, two-zone tandem mirror blanket designed for the dual applications of high efficiency electricity production or process heat for synthetic fuel production is presented. The blanket is self-sufficient in tritium production, delivers 46% of the blanket energy at 900 to 1000°C, meets guidelines for near-surface burial of radioactive wastes and couples to a power cycle that has a net efficiency of 44%. The design is based on a new concept of a dilute mixture of a solid breeder with a high temperature material that extends the temperature range of the breeder. The low temperature zone is Li17Pb83 cooled while the high temperature zone is cooled with helium.