航空兵器Issue(3)：40-43,4.
高温条件下 HTPB 推进剂药柱老化研究
Research on Grain Aging of HTPB Propellants under the High Temperature Condition
曹亮 1于晓辉 1徐波 2杜向辉 1左艳辉 1高胜臣1
作者信息
- 1. 海军驻洛阳地区航空军事代表室，河南洛阳 471009
- 2. 91467部队山东胶州 266311
- 折叠
摘要
Abstract
For the problem of the composite solid propellant aging , the aging mechanism and the main aging influencing factors of the composite solid propellant are discussed .Based on a certain compos-ite solid propellant grain , accelerated aging experiment in high temperature condition are set up .By re-searching the storage stability of HTPB propellant under the high temperature and accelerated aging condi -tions, the changing rule of all storage stability following the aging time is gotten ,and the aging mechanism of HTPB propellant in high temperature and accelerated aging conditions is analysed , the life of HTPB propellant grain is estimated.关键词
复合固体推进剂/加速老化/老化机理/寿命预估Key words
composite solid propellant/accelerated aging/aging mechanism/life estimate分类
航空航天引用本文复制引用
曹亮,于晓辉,徐波,杜向辉,左艳辉,高胜臣..高温条件下 HTPB 推进剂药柱老化研究[J].航空兵器,2014,(3):40-43,4.
