The nuclear ramjet propulsion system
Theodore C. Merkle, Lawrence Livermore Laboratory, University of California, Berkeley. Lawrence Radiation Laboratory
University of California Radiation Laboratory, 1961 - Technology & Engineering - 20 pages
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aerodynamic requirements air stream amount of fuel annoying problem atom chemical core duct contain employee or contractor Exit end fabricated fast reactor fission activity fission cross section fission fragments fission product flight Mach number forces the develop fuel elements Furthermore gram of fission heat exchanger heat transfer heat-exchanger wall heterogeneous reactor High-pressure piping High-temperature ceramic homogeneous moderated reactor homogeneous reactor hot moderator II-A series inlet end intermetallic compounds large excess reactivity Lawrence Radiation Laboratory lb of air Livermore load megawatts nuclear fuel NUCLEAR RAMJET PROPULSION nuclear ramjet reactor number proportional operate pressure duct process disclosed PROPULSION SYSTEM Theodore ramjet engine reactor ramjet missile ramjet power plants ramjet propulsion systems reactor design reactor is selected reactor radiations reactor wall temperature reasonable reactor reflector relations between flight requirements of flight sea level slow neutrons slow the neutrons suitable tension tubes test vehicle thrust coefficient Tory II-A-1 Tory II-C uranium