首页|固体火箭发动机低易损技术研究进展

固体火箭发动机低易损技术研究进展

扫码查看
基于国外低易损固体推进剂研究,对低易损性概念、低易损固体火箭发动机关键技术现状,以及低易损性试验标准、缩比试验方法、仿真模拟等进行了综述分析.对国内低易损技术理论研究需完善的问题,从数值模拟仿真、新型低易损推进剂研制、固体火箭发动机设计技术、低易损试验表征技术及相关评价等方面提出了技术建议.
Research progress of low vulnerability technique for solid rocket motor
Based on the research of low vulnerability solid propellants abroad,the concept of low vulnerability,the current status of key technologies of low vulnerability solid rocket motor,as well as low vulnerability test standards,small-scale test methods,simulations,etc.are reviewed and analyzed.In view of the problems that need to be perfected in the theoretical research of domestic low vulnerability techniques,technical suggestions are put forward from the aspects of numerical simulations,development of new type of low vulnerability propellants,design techniques of solid rocket motor,characterization techniques of low vulnerability tests,related evaluations,etc.

low vulnerability solid propellantsolid rocket motorevaluation

胡丰泽、冀占慧、高建兵、王佳、郝平、马鹤

展开 >

海军装备部,内蒙古包头 014000

内蒙合成化工研究所,内蒙古呼和浩特 010010

低易损固体推进剂 固体火箭发动机 评估

2024

化学推进剂与高分子材料
黎明化工研究院有限责任公司

化学推进剂与高分子材料

影响因子:0.289
ISSN:1672-2191
年,卷(期):2024.22(2)
  • 44