固体火箭技术2004，Vol.27Issue(4)：298-303,6.
固体火箭发动机预固化技术及其应用
Pre-cure Technique and Its Applications for Solid Rocket Motors
苏昌银 1张爱科1
作者信息
- 1. The No.7416 Factory of the Fourth Academy of CASC, Xi'an 710072, China
- 折叠
摘要
Abstract
Based on interface properties of HTPB propellant, the cross linking level is regulated through the temperature and time of cure reaction. The chemical reaction takes place gradually in remainder functional groups of the system to form chemical bonds and hydrogen bond, so as to improve the mechanical properties of the resultant. Pre-cure technique and bonding model are described in the paper. They can be used in propellant-liner bonding, propellant loading and integral repairing of the propellant grain of the solid rocket motor (SRM). These test results have been qualified by the successful static firing tests, flight tests of motors and storage tests of specimens for ten-years. The performances of the motor meet the design requirements with good reproducibilities.关键词
solid rocket motor/pre-cure technique/HTPB propellantKey words
solid rocket motor/pre-cure technique/HTPB propellant分类
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苏昌银,张爱科..固体火箭发动机预固化技术及其应用[J].固体火箭技术,2004,27(4):298-303,6.
