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Nonequilibrium Recombination in Nozzles: Fundamental Recombination Processes in Loxhydrogen, Flourine-Hydrogen, and Flox-Hydrogen Propellants

机译：喷嘴中的非平衡重组：Loxhydrogen，Flourine-Hydrogen和Flox-Hydrogen推进剂中的基本重组过程

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The significant nozzle recombinattion steps are tabulaated for combustion products formed by LOX-hydrogen, fluorine-hydrogen, and FLOX-hydrogen propellants. Kinetic data for each of these 23 nozzle reactions are summarized. A systematic basis is presented for selecting the significant nozzle reactions of atoms, radicals, and molecules for inclusion on the data tapes of computer programs for nonequilibrium calcuclculations of propelellant performance. Thhe relative importance of the pre-exponential factor in high-temperature recombinations is emphasized. A method is given for reducing the number of equations needed in nonequilibrium performance calculations involving termolecular recombinations. A procedure for calculating concentrations of light-emitting excited states in the exhaust is presented. Ionization constants for the formation of cations, anions, and electrons in nozzle gases are computed and discussed briefly. (Author)

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Mayer, S. W.; Cook, E. A.; Schieler, L.;
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年度 1964
页码 p.1-2
总页数 2
原文格式 PDF
正文语种 eng
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关键词
ROCKET PROPELLANTS ; COMBUSTION PRODUCTS ; ROCKET MOTOR NOZZLES ; RECOMBINATION REACTIONS ; EXHAUST GASES ; LIQUEFIED GASES ; OXYGEN ; FLUORINE ; HYDROGEN ; REACTION KINETICS ; ATOMS ; MOLECULES ; FREE RADICALS ; GAS IONIZATION ; PLASMA MEDIUM ; CHEMICAL EQUILIBRIUM ; PROGRAMMING (COMPUTERS);

机译：火箭推进剂;燃烧产物;火箭发动机喷嘴;重组反应;排气;液化气体;氧气;氟;氢;反应动力学;原子;分子;自由基;气体电离;等离子体介质;化学平衡;程序设计（计算机）;

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7. Influence of Heterogeneous Reaction Processes on Atomic Recombination Rates in Rocket Nozzles [O] . Penner S. S., Porter J. W. 1962

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8. Nonequilibrium Rocket Nozzle Recombination Losses [R] . Cook, E. A., Schieler, L. 1964

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Nonequilibrium Recombination in Nozzles: Fundamental Recombination Processes in Loxhydrogen, Flourine-Hydrogen, and Flox-Hydrogen Propellants

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