PURPOSE: To surely suppress corrosion particularly in a nozzle throat part also to cool this part so as to improve propulsive performance by making as the basis that a contracting cylinder part in the upstream of the nozzle throat part is formed of a fiber reinforced plastic-made nozzle member...
The nozzleless solid rocket motor is a new type of motor which differs from the traditional motor, refers to many subjects and has a very complex system process. 无喷管固体火箭发动机是一种区别于传统发动机的新型火箭发动机,它涉及到的基础知识面广,系统工作过程复杂。3) solid nozzle 固体燃料火箭...
nozzleless-solid-rocket-motor网络无喷管固体火箭发动机 网络释义 1. 无喷管固体火箭发动机 无喷管固体助推器,NSRB,音标,读... ... ) nozzleless solid rocket motor 无喷管固体火箭发动机 ) booster nozzle 助推器喷管火> ... www.dictall.com|基于1 个网页©...
PURPOSE: To surely suppress corrosion particularly in a nozzle throat part also to cool this part so as to improve propulsive performance by making as the basis that a contracting cylinder part in the upstream of the nozzle throat part is formed of a fiber reinforced plastic-made nozzle member...
关键词:固体推进剂火箭发动机;喷管;计算机辅助设计;流场; 烧蚀;有限元法 中图分类号:V435文献标识码:A Theintegrateddesignandanalysisofsolidrocketmo- tornozzles BAOFu-ting,GUODa-ing,ZHAOFei,LIUJun-ping !Co egeofAstronauticsofNorthwesternPo ytechnica University, Xi'an710072,China. Abstract:Theconfiguratio...
solid rocket motor Linguee +人工智能=DeepL翻译器 翻译较长的文本,请使用世界上最好的在线翻译! ▾ 英语-中文正在建设中 solid形— 固体形 · 坚实形 · 扎实形 · 牢固形 · 固含量形 solid— 实 · 寔 rocket名— 箭名 · 火箭名 · 火箭弹名...
A solid propellent motor comprised of a metal casing for containing the solid propellent charge, a thin wall nozzle formed of carbon or graphite fibers or filaments, disposed in a carbon or graphite binder; the nozzle is affixed to the high strength case by an elongated transition section formed...
为了满足固体火箭发动机喷管一体化的粘接要求,提高产品的粘接质量,分析了胶粘剂性能、粘接工艺、温度及内衬与壳体的配合间隙对喷管粘接质量的影响,结果表明,通过控制影响一体化喷管粘接的各种因素,得出了最佳的工艺生产条件,保证了发动机工作的可靠性。 关键词: 喷管;一体化;粘接工艺 ...
SOLID PROPELLENT ROCKET MOTOR NOZZLE 专利名称：SOLID PROPELLENT ROCKET MOTOR NOZZLE 发明人：RICHARD L. BAILEY,WARREN L.DOWIER,JOHN I. SHAFER 申请号：US3648461D 申请日：19700513 公开号：US3648461A 公开日：19720314 专利内容由知识产权出版社提供 摘要：A solid propellent motor comprised of a metal ...
4)Solid propellant rocket motor固体火箭发动机 1.Contour design and numerical calculation of certain solid propellant rocket motor nozzle;某型号固体火箭发动机喷管型面设计与数值计算 2.Thrust Vector Control (TVC) system of certain type solid propellant rocket motor was the research object and multibody dy...