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The book J.G.Demjanko, A.S.Koroteyev's , etc. " Nuclear Rocket Engines ",
2001 is published in Russia.. This book is interesting that it data from technological reports (probably, before "confidential") of some scientific organizations of the USSR and Russia on series and purposeful creation of a nuclear rocket engine 11B91-IR-100 with a thrust about 3,6 tons and power about 3-10 megawatt are adduced. These activities have begun in 50th years and proceeded until recently. On May, 28, 2000 for this reactor S.Zaletnyj and A.Kaleri astronauts during the flight on "MIR" space stations are tested the drop refrigerator for the program "Sheet - 2" which provides a scoring on weight near 90 tons in comparison with conventional radiators. Physical models of nuclear rocket engine were tested on "Baikal - 1"stand ( Semipalatinsk range) and on existing bench "Strela" in Physics-Power Institute. Physical launch has been made on March, 27 1978. Practically everything, including the design documentation on manufacturing nuclear rocket engine 11B91-IR-100 is made, what's why the center of Keldysh (Russia) offers this engine as the base engine for future Martian expeditions. Adron V. Pon |
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