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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.
Jan S. Brzosko, Jean Pierre Rager, B. V. Robouch, Achim H. Bähr, Hans Volker Klapdor, Erling Andersson, Peter Herges
Fusion Science and Technology | Volume 4 | Number 2 | September 1983 | Pages 263-276
Technical Paper | Special Section Content / Experimental Device | doi.org/10.13182/FST83-A22818
Articles are hosted by Taylor and Francis Online.
The ratio R(D-D)/R(D-3He) of yields of fusion reactions was used as a diagnostic tool for studying the effective ion energy of plasma produced in the 1-MJ plasma focus device at Frascati. The device is operated in the neutron-optimized mode at energies of 250, 390, and 490 kJ. The reaction yields are determined by measuring the activity induced in the 63 Cu(p,n)63 Zn (Ep = 14.6 MeV) and 115 In(n,n')115m In (En = 2.45 MeV) reactions. A detailed discussion of the energy slowing down of neutrons is given and a new calibration of the (p,n) cross section of the monitor reaction is performed. The measurements are carried out simultaneously for the end-on and side-on positions, and no significant differences are observed. A comparison with other experimental data is given. Conversion of the ratio of fusion reaction yields to ion temperatures or effective ion energies of streams interacting with a cold gas medium gives kTt ≅ 14 keV or Ed(kTe = 0.5 keV) = 72 keV, respectively.