| 摘要: |
| 本文主要介绍90N和490N两种四氧化二氮/一甲基肼推力室的设计及试验概况. |
| 关键词: 液体推进剂火箭发动机 姿态控制 推力室 |
| DOI： |
| 分类号: |
| 基金项目: |
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| RESEARCH ON N2O4/MMH THRUSTER |
|
Zu Lingen1, Zhong Mingli2
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1.The 11st Research Institute;2.The 12st Research Institute
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| Abstract: |
| In this paper the design and the test of two N2O4/MMH thru-sters,with thrust of 98N or 490N, are chiefly described. |
| Key words: Liquid rocket engine Attitude control Thrust chamber |
