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Research of formulation and processing of hydroxyl-terminated polybutadiene (HTPB) propellants

  • Slimane Bekhouche*
  • , Yun Jun Luo
  • *此作品的通讯作者
  • Beijing Institute of Technology

科研成果: 书/报告/会议事项章节会议稿件同行评审

摘要

Solid composite propellants are extensively used for propulsion of rockets, missiles and space applications. The composite propellant is a polymeric matrix in which the oxidizer and fuel particles are embedded in a polymeric binder. Different composite propellant mixtures have been prepared using ammonium-perchlorate (ratio 70:30) as oxidant and mixture of aluminium powder (ratio 50:50) as metal component. In the present work, RDX (Cyclotrimethylene trinitramine) has been used in successive increments replacing AP (Ammonium Perchlorate) in number of batches by varying the percentage of solid loading, and studied their different properties such as viscosity build-up, mechanical and ballistic properties.

源语言英语
主期刊名Materials, Transportation and Environmental Engineering II
编辑Jimmy C.M. Kao, Wen-Pei Sung, Ran Chen
出版商Trans Tech Publications Ltd.
155-160
页数6
ISBN(电子版)9783038352488
DOI
出版状态已出版 - 2014
已对外发布
活动2nd International Conference on Materials, Transportation and Environmental Engineering, CMTEE 2014 - Kunming, 中国
期限: 30 7月 201431 7月 2014

出版系列

姓名Advanced Materials Research
1030-1032
ISSN(印刷版)1022-6680
ISSN(电子版)1662-8985

会议

会议2nd International Conference on Materials, Transportation and Environmental Engineering, CMTEE 2014
国家/地区中国
Kunming
时期30/07/1431/07/14

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