Nuclear-pulse propulsion
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Advantages of Fast Ignition Scenarios with Two Hot Spots for Space Propulsion Systems
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Creation of the Directed Plasma Fluxes with Ignition of Microexplosions by and with the use of Distant Microexplosions
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Some Thermonuclear Power Plants as the Possible Sources of He3 for Space Propulsion Systems
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Starfleet Deferred: Project Orion in the 1962 Air Force Space Program
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The Expected Efficiency of Burning of the D-He3 Fuel in Space Propulsion Systems
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The Moon and the Medusa – Use of Lunar Assets in Nuclear-Pulse-Propelled Space Travel
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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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