中国空间科学技术

中国空间科学技术

• •    

剩余推进剂排放系统研究

廖少英   

  1. 上海航天局机电设备研究所!上海200245
  • 发布日期:2001-02-25

Research of the Residual Propellant Dumping System

Liao Shaoying (Machine-Electron Equipment Research Institute,Shanghai 200245)   

  • Online:2001-02-25

被引次数

3

摘要： 论述中国首枚上面级火箭剩余推进剂排放方案论证 ,排放系统方案选择 ;提出中国专用排放系统方案 ,排放系统设计、研制与试验研究的全过程 ,为解决中国长征型号上面级火箭高空爆炸解体问题提供了技术基础

关键词: 推进剂剩余量, 排放系统, 研究, 航天器

Abstract: The dumping scheme demonstration and option of the residual propellant of first upper stages rocket of China are discussed.The scheme of dumping system for special use is put forward.The design,development and experiment of all process is introduced.Based on the technology,the problem of explosive disintegrate in the high altitude of upper stage rocket of Long March Model Vehicles is expected to be solved.