Tang Chenghu, Qiang Hongfu, Geng Tingjing, Wang Xueren, Zhang Feng
Zhijian Laboratory, Rocket Force University of Engineering, Xi'an 710025, China.
School of Aerocraft, Xihang University, Xi'an 710077, China.
Polymers (Basel). 2025 Jul 26;17(15):2039. doi: 10.3390/polym17152039.
Solid propellant grain, as a typical polymer, are the thrust generation devices and core load-bearing components of solid rocket motor (SRM) and are also known as SRM grain. They are constantly exposed to extreme service environments such as high temperatures, high pressures, and dynamic shocks, and have a relatively high failure rate in the field use of SRM. Its life and reliability are the shortcomings that restrict the improvement of weapons and equipment capability in China at present. This paper summarizes the typical fault types of SRM grain at present, and compares and analyzes the research progress of reliability design and analysis technology, reliability optimization technology, life test technology and reliability evaluation technology of SRM grain at home and abroad; This paper analyzes the deficiencies and reasons in the research and application of SRM grain reliability technology in China, and points out the technical difficulties and challenges faced by the integrated design of performance and reliability of SRM independent innovation design according to the needs of the forward research and development system of SRM. Based on the existing design level and industrial foundation in China, the basic research suggestions that should be carried out to consolidate the design ability of SRM grain in China are given.
固体推进剂药柱作为一种典型的聚合物,是固体火箭发动机(SRM)的推力产生装置和核心承载部件,也被称为SRM药柱。它们不断暴露于高温、高压和动态冲击等极端服役环境中,在SRM的实际使用中故障率相对较高。其寿命和可靠性是目前制约我国武器装备性能提升的短板。本文总结了目前SRM药柱的典型故障类型,对比分析了国内外SRM药柱可靠性设计与分析技术、可靠性优化技术、寿命试验技术和可靠性评估技术的研究进展;分析了我国SRM药柱可靠性技术研究与应用中的不足及原因,并根据SRM预先研究发展体系的需求,指出了SRM自主创新设计中性能与可靠性一体化设计面临的技术难点与挑战。基于我国现有的设计水平和产业基础,给出了巩固我国SRM药柱设计能力应开展的基础研究建议。