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[1]李淑艳,肖明杰,李晓瑾,等.新型活塞泵增压轨/姿控发动机系统方案研究[J].火箭推进,2012,38(01):12-16.
　LI Shu-yan,XIAO Ming-jie,LI Xiao-jin,et al.Scheme study on divert and attitude control engines with piston pump pressurized system[J].Journal of Rocket Propulsion,2012,38(01):12-16.
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新型活塞泵增压轨/姿控发动机系统方案研究

《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V] 卷: 38 期数: 2012年01期 页码: 12-16 栏目: 研究与设计 出版日期: 2012-02-15
Title:
Scheme study on divert and attitude control engines with piston pump pressurized system
文章编号:
1672-9374(2012)01-0012-06
作者:
李淑艳; 肖明杰; 李晓瑾; 郑小鹏; 董万峰
西安航天动力研究所，陕西 西安 710100
Author(s):
LI Shu-yan;  XIAO Ming-jie;  LI Xiao-jin;  ZHENG Xiao-peng;  DONG Wan-feng
Xi’an Aerospace Propulsion Institute, Xi’an 710100, China
关键词:
活塞泵; 增压系统; 轨/姿控发动机
Keywords:
piston pump;  pressurized system;  divert and attitude control engine
分类号:
V434-34
文献标志码:
A
摘要:
介绍了国外新型活塞泵增压轨/姿控发动机系统发展现状，提出了一种新型活塞泵增压轨/姿控发动机系统方案，介绍了新型活塞泵增压轨/姿控发动机系统特点并分析了新型发动机系统关键技术，开展了新型活塞泵增压轨/姿控发动机系统研究，掌握了主要组件设计技术，获得了活塞泵增压系统仿真特性。
Abstract:
The development of foreign piston pump pressurized systems for the divert and attitude control engines is narrated. A new scheme of divert and attitude control engine with a piston pump pressurized system is brought out. The system characteristics are introduced and the key technologies are analyzed. The scheme of a new piston pump pressurized system for divert and attitude control engines is studied. The design technologies of main components have been mastered. The simulation characteristics of the piston pump pressurized system were obtained.

相似文献/References:

[1]朱建国,曾维亮,董万峰.基于流体逻辑理论的某活塞泵逻辑特性分析[J].火箭推进,2013,39(03):93.
　ZHU Jian-guo,ZENG Wei-liang,DONG Wan-feng.Analysis on logic behaviour of a piston pump based on fluid logic theory[J].Journal of Rocket Propulsion,2013,39(01):93.
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备注/Memo

收稿日期：2011-10-13；修回日期：2011-11-16
基金项目：总装备部预研项目（2009AA702051）
作者简介：李淑艳（1980—），女，工程师，研究领域为液体火箭姿/轨控发动机系统设

更新日期/Last Update: 1900-01-01