Currently, C/C composites have become a widely used ablative thermal protection material in solid rocket motor nozzle design due to their excellent properties such as high strength, good ablative resistance, and very high impact resistance. This study develops a dual-region solid rocket motor C/C...
Solid rocket motorDesign and fabrication of a tactical motor nozzle flexible joint were accomplished in this paper. The miniature flexible joint configuration characteristics were analyzed. The silicone rubber was selected as the elastomer ring material based on the mechanical properties test. Individual ...
Design of a Solid Rocket Motor for an Air to Air Missile:一个空空导弹固体火箭发动机设计 大型固体火箭喷管与燃烧室对接装置及方法 固体火箭发动机喷管的设计与性能仿真 固体火箭发动机长尾喷管内流场特性研究 某型号固体火箭发动机喷管型面设计与数值计算 固体火箭发动机C/C复合材料喷管烧蚀行为建模仿真方法 固体火箭...
Rocket motor nozzlesTocket propellent grainsRocket ignitersThe pamphlet is devoted to description of working principle of solid propellent rocket engines and ... VV Pozhkov 被引量: 0发表: 1965年 Development of a rocket recovery system The parachute recovery system constructed in this project will ...
5) rocket nozzle 火箭发动机喷管 例句>> 6) solid rocket motor 固体火箭发动机 1. Grain design of solid rocket motor based on ACIS geometric modelling platform; 基于ACIS几何造型平台的固体火箭发动机装药设计 2. Analysis on fluid-structural coupling of solid rocket motor during rapid pressurization...
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 casing for containing the solid ...
Design of solid rocket motor becomes an exigent task when accounting for chamber design, nozzle design, ballistic performance calculations as well as grain geometry and regression. CAD modeling overcomes the limitation posed by analytical expression thus increased model fidelity. CAD model allows ...
Rockets, rocket propulsion systems, MLRS G-2000 122mm, gas turbines, anti-tenk, anti-ship, surface-to-surface, surface-to-air, air-to-surface & cruise missile
Design of a Solid Rocket Motor for an Air to Air Missile:一个空空导弹固体火箭发动机设计 热度: 文章编号:1006-2793(2002)02-0025-03 某固体发动机反向喷管型面优化设计 ! 张四清 (中国三江航天集团精密机械研究所,武汉430034) 摘要:某固体发动机推力终止装置结构空间十分有限,为保证推力终 ...
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©...