M.L. Shmatov
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Advantages of Fast Ignition Scenarios with Two Hot Spots for Space Propulsion Systems
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Some Problems Related to Safety and Efficiency of the use of Antihydrogen and Antiprotons
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Some Thermonuclear Power Plants as the Possible Sources of He3 for Space Propulsion Systems
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Space Propulsion Systems Utilising Ignition of Microexplosion by Distant Microexplosion….
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The Typical Number of Antiprotons Necessary to Heat the Hot Spot in the D-T Fuel Doped with U
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