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FEASIBILITY OF OPTIMIZING NOZZLE PERFORMANCE FOR ORBITALLAUNCH NUCLEAR ROCKETS

机译：优化核弹头核弹簧喷嘴性能的可行性

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Feasibility of optimizing nozzle performance for orbital-launch nuclear rockets

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作者
Jack, J. R.;
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年度 1963
页码 1-26
总页数 26
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
HEAT TRANSFER; NUCLEAR ROCKET ENGINES; ORBITAL LAUNCHING; ROCKET NOZZLES; THROATS; NUCLEAR ROCKET; ORBITAL LAUNCH; ROCKET NOZZLE;

机译：传播热量;核弹簧发动机;轨道发射;火箭喷嘴;喉咙;核火箭; ORBITaL LaUNCH;火箭喷嘴;

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1. A feasibility study on low enriched uranium fuel for nuclear thermal rockets - II: Rocket and reactor performance [J] . Venneri Paolo F., Kim Yonghee Progress in Nuclear Energy . 2016,第Mara期

机译：核热火箭用低浓铀燃料的可行性研究-II：火箭和反应堆性能
2. OPTIMIZATION OF COMPRESSION MOULDING PROCESS PARAMETERS TO ENHANCE THE PERFORMANCE OF SOLID ROCKET NOZZLE CONVERGENT LINERS USING TAGUCHI'S ROBUST DESIGN METHODOLOGY [J] . N. Kishore Nath MTT: Manufacturing Technology Today . 2015,第8期

机译：用Taguchi的稳健设计方法优化压缩成型工艺参数以提高固体火箭喷嘴会聚衬里的性能。
3. Performance prediction and optimization for liquid rocket engine nozzle [J] . Guobiao Cai, Jie Fang, Xu Xu, Aerospace science and technology . 2007,第2a3期

机译：液体火箭发动机喷嘴性能预测与优化
4. Feasibility Studies on the Cooling of Hybrid Rocket Nozzles using Supercritical Nitrous Oxide [C] . Abhinav Kumar, Vishnu Saini, Preeti Rao Usurumarti International Conference on Recent Advancement in Air Conditioning and Refrigeration . 2017

机译：使用超临界二氧化二氮氧化物冷却混合火箭喷嘴的可行性研究
5. Design and CFD optimization of methane regenerative cooled rocket nozzles. [D] . Bradford, Christopher Linn. 2011

机译：甲烷可再生冷却火箭喷嘴的设计和CFD优化。
6. Optimization and evaluation of Luminex performance with supernatants of antigen-stimulated peripheral blood mononuclear cells [O] . Mathieu Surenaud, Céline Manier, Laura Richert, 2016

机译：抗原刺激的外周血单核细胞上清液对Luminex性能的优化和评估
7. Analytical study of nozzle performance for nuclear thermal rockets [O] . Davidian, Kenneth O., Kacynski, Kenneth J. 1991

机译：核热火箭喷嘴性能的分析研究

FEASIBILITY OF OPTIMIZING NOZZLE PERFORMANCE FOR ORBITALLAUNCH NUCLEAR ROCKETS

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