某型固体火箭发动机综合性能试验与寿命评估

推进技术 ›› 2004, Vol. 25 ›› Issue (2): 176-179.

某型固体火箭发动机综合性能试验与寿命评估

邢耀国,金广文,许学春,侯本学,刘海峰,董可海

海军航空工程学院;山东烟台264001;海军航空工程学院;山东烟台264001;92941部队;辽宁葫芦岛125001;海军装备部驻北京星航机电设备公司军代室;北京100074;海军航空工程学院;山东烟台264001;海军航空工程学院;山东烟台264001

发布日期:2021-08-15
基金资助:
总装备部"十五"预研项目(41328010507)。

Comprehensive property tests and service life evaluation for solid rocket motors

Naval Aeronautical Inst., Yantai 264001, China;Naval Aeronautical Inst., Yantai 264001, China;Troops of 92941, Huludao 125001, China;Militant Representalives Office of Naval Dept. in Beijing Xinghang Electro-Mechamical Equipment Corp., Beijing 100074, China;Naval Aeronautical Inst., Yantai 264001, China;Naval Aeronautical Inst., Yantai 264001, China

Published:2021-08-15

摘要/Abstract

摘要： 对不同贮存期的某型固体火箭发动机进行了零部件的功能试验和燃烧室的解剖试验。根据试验测得的推进剂化学性能和力学性能的变化,对不同贮存期的发动机进行了内弹道和结构完整性计算。比较理论分析和综合性能试验的结果,对该型发动机服役寿命进行了评估,发现决定其寿命的因素是粘接界面的失效。

关键词: 固体推进剂火箭发动机;性能试验;寿命预测;内弹道模拟计算;结构完整性

Abstract: The functional tests of the parts and units and the dissection tests of the combustion chambers had been done for the solid rocket motors which were in variable storage times. According to the change of the chemical properties and the mechanical properties obtained from the tests, the simulation of interior ballistic and the structural integrity analysis for these motors were conducted. By investigating the results from the theoretical analysis and the comprehensive property tests,the service life of these motors were evaluated and it was found that the factor determing the service life of these motors is the misfunction of the binding interfaces.

Key words: Solid propellant rocket engine;Performance test;Life prediction;Interior ballistic simulation calculation;Structural integrity

邢耀国,金广文,许学春,侯本学,刘海峰,董可海. 某型固体火箭发动机综合性能试验与寿命评估[J]. 推进技术, 2004, 25(2): 176-179.