E-resources
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Chernyshev, V.K.; Mokhov, V.N.; Buzin, V.N.; Burenkov, O.M.; Bujko, A.M.; Vakhrushev, V.V.; Garanin, S.F.; Grinevich, B.E.; Gorbachev, Y.N.; Demidov, V.A.; Dudoladov, V.I.; Zmushko, V.V.; Kuzyaev, A.I.; Kucherov, A.I.; Lovyagin, B.M.; Matsev, Y.I.; Nizovtsev, P.N.; Petrukhin, A.A.; Pishchurov, A.I.; Sokolov, S.S.; Solovjov, V.P.; Startsev, A.I.; Yakubov, V.B.; Anderson, B.G.; Ekdahl, C.A.; Gofort, D.; Clark, D.; Lindemuth, I.R.; Reinovsky, R.E.; Fail, R.; Younger, S.M.
Digest of Technical Papers. 11th IEEE International Pulsed Power Conference (Cat. No.97CH36127), 1997, Volume: 1Conference Proceeding
The paper describes arrangement and the results of the first joint experiment between VNIIEF and LANL with explosive magnetic generators (EMG) of 1 m diameter and a nonevaporating liner. The experiment took place in August 22, 1996. The goal of the experiment was to accelerate magnetically cylindrical relatively thin aluminum liner and to get kinetic energy of 20 MJ or more. As the energy source for the experimental device we chose 5-module DEMG of 1000 mm diameter, tested many times in the experiments for rigid and liner loads. This EMG can store more energy than any other EMG created at VNIIEF. The physical scene of the liner unit was chosen so that the growth of disturbances would have less influence on the liner shape during flight, especially on the liner's inner surface. The shape of glade plane on which the liner slides during flight and the way of contact liner with walls were chosen on the grounds of 2-D calculations, proceeding from the necessity to ensure electrical contact during the liner flight.
