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• W255504404 abstract "Publisher Summary This chapter presents a review of the potential applications of nuclear and solar energy for propulsion of spacecraft. The basic methods of thrust generation fall into four categories. The first method utilizes direct heating of a working fluid. The second and third require that electrical power be generated and then transferred to a propellant, either as thermal energy or as directed kinetic energy. The fourth requires that mechanical power be generated and applied to impart energy to a propellant by compression, prior to nozzle expansion. The use of nuclear fission energy for direct heating of a rocket propellant might occur with a nuclear reactor containing a fissionable material. The propellant should have a rapid rate of recombination for dissociated atoms or free radicals, which might be formed in the reactor in order that the recombination energy might be converted to kinetic energy in a nozzle of reasonable length." @default.
• W255504404 created "2016-06-24" @default.
• W255504404 creator A5084333011 @default.
• W255504404 date "1961-01-01" @default.
• W255504404 modified "2023-09-27" @default.
• W255504404 title "Advanced Nuclear and Solar Propulsion Systems" @default.
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• W255504404 doi "https://doi.org/10.1016/b978-1-4831-9961-0.50012-2" @default.
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