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Composite Solid Rocket Propellant Based on GAP Polyurethane Matrix with Different Binder Contents

Islam K .Boshra Ahmed Elbeih GUO Lin Mohamed G .Zaki

火炸药学报2020，Vol.43Issue(4)：362-367,6.

火炸药学报2020，Vol.43Issue(4)：362-367,6.DOI:10.14077/j.issn.1007-7812.202004022

Composite Solid Rocket Propellant Based on GAP Polyurethane Matrix with Different Binder Contents

Islam K .Boshra ¹Ahmed Elbeih ²GUO Lin ¹Mohamed G .Zaki²

作者信息

1. School of Chemistry and Environment ,Beihang University ,Beijing 100191 ,China
2. Military Technical College ,Kobry Elkobbah ,Cairo ,Egypt
折叠

摘要

关键词

physical chemistry/glycidyl azide polymer (GAP)/hydroxyl terminated polybutadiene (HTPB)/cross-linker/me-chanical properties

Key words

physical chemistry/glycidyl azide polymer (GAP)/hydroxyl terminated polybutadiene (HTPB)/cross-linker/me-chanical properties

分类

军事科技

引用本文复制引用

Islam K .Boshra,Ahmed Elbeih,GUO Lin,Mohamed G .Zaki..Composite Solid Rocket Propellant Based on GAP Polyurethane Matrix with Different Binder Contents[J].火炸药学报,2020,43(4):362-367,6.

火炸药学报

OA北大核心CSCDCSTPCD

ISSN：1007-7812

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