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[1]任建军.国外空间攻防武器动力系统技术发展概述[J].火箭推进,2012,38(01):7-11.
　REN Jian-jun.Overview of technology development of propulsion systems for space attack and defense weapons abroad[J].Journal of Rocket Propulsion,2012,38(01):7-11.
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国外空间攻防武器动力系统技术发展概述

《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V] 卷: 38 期数: 2012年01期 页码: 7-11 栏目: 专论与综述 出版日期: 2012-02-15
Title:
Overview of technology development of propulsion systems for space attack and defense weapons abroad
文章编号:
1672-9374(2012)01-0007-05
作者:
任建军
上海空间推进研究所，上海201112
Author(s):
REN Jian-jun
Shanghai Institute of Space Propulsion, Shanghai 201112, China
关键词:
空间攻防武器; 动力系统
Keywords:
space attack and defense weapon;  propulsion system
分类号:
V434-34
文献标志码:
A
摘要:
概述了空间攻防武器动力系统研究的重要意义、国外发展情况以及突破的姿/轨控发动机及阀门、贮箱、系统增压等关键技术，并对未来向轻小型化、快响应、高性能、预包装、低冰点、凝胶推进剂和无毒化等方向发展做了预测。
Abstract:
The importance of investigating the propulsion systems for space attack and defense weapons is outlined. The development and breakthrough of key technologies such as orbit/attitude control engine, valves, tanks and pressurization system are elaborated. The developing directions of light miniaturization, fast response and high performance propulsion systems, and pre-packaging, low freezing point, non-toxic and gel propellants are predicted.

参考文献/References:

[1]张宏安, 叶定友, 郭彤. 固体动能拦截器研究初探[J]. 固体火箭技术, 2002(4): 6-8.
[2]李世鹏, 张平. 轻型动能拦截器固体控制发动机方案分析[J]. 推进技术, 1999, 20(2): 99-102.
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[8]REED Brian. Material compatibility testing with HAN-based monopropellants, AIAA2001-3696[R]. USA: AIAA, 2001.
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备注/Memo

收稿日期：2011-05-12；修回日期：2011-08-29
作者简介：任建军（1979—），男，工程师，研究领域为空间推进系统研制

更新日期/Last Update: 1900-01-01