惰性丁羟固体推进剂研制

推进技术 ›› 1996, Vol. 17 ›› Issue (2): 77-81.

惰性丁羟固体推进剂研制

沈希,缪惟英,戴耀松,段清廉

航天工业总公司３１所;航天工业总公司３１所;航天工业总公司３１所;航天工业总公司３１所

发布日期:2021-08-15

DEVELOPMENT OF INERT HTPB SOLID PROPELLANT

The 31st Research Inst.,Beijing,100074;The 31st Research Inst.,Beijing,100074;The 31st Research Inst.,Beijing,100074;The 31st Research Inst.,Beijing,100074

Published:2021-08-15

摘要/Abstract

摘要： 介绍一种惰性丁羟推进剂的基础配方及其制造方法。所研究的惰性丁羟推进剂的力学性能与真实推进剂相当，从而可替代真实推进剂，广泛用于固体火箭发动机的环境试验、全弹调试测量以及阅兵、展览等场合。

关键词: 端羟基聚丁二烯推进剂;惰性材料;模拟装药

Abstract: basic formulatiot and manufacturing method of on inert HTPB solid propellent is introducde.The result shows that the mechanic properties of the inert HTPB solid propellant is correspond to the real one .This kind of inert propellant can be used to replace real propellant in enviroment test of the solid rocket motor,adjustment and measurement of complet missiles and military review and exhibition.

Key words: Hydroxy terminated polybutadiene propellant;Inert material;Simulated charge

沈希,缪惟英,戴耀松,段清廉. 惰性丁羟固体推进剂研制[J]. 推进技术, 1996, 17(2): 77-81.