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中国航天固体火箭技术的发展

叶定友 张德雄

固体火箭技术2002,Vol.25Issue(2):1-7,7.
固体火箭技术2002,Vol.25Issue(2):1-7,7.

中国航天固体火箭技术的发展

Evolution of Chinese solid rocket propulsion technology for space missions

叶定友 1张德雄1

作者信息

  • 1. 中国航天科技集团公司四院,西安,710025
  • 折叠

摘要

Abstract

The evolution course of Chinese solid rocket propulsion technology for space missions since 1950s is presented.The technical features,development process,ground tests and flight records of nine typical solid motors are described.These motors were developed for sounding rockets,upper stages of launch vehicles and orbit transfer systems in application satellites respectively.The evolution of basic technology of Chinese solid rocket motors and future developing concept are briefly introduced.The information in the paper are all based on the published literatures.

关键词

固体推进剂火箭发动机/中国/火箭推进/探空火箭/运载火箭

Key words

solid propellant rocket engine/China/rocket propulsion/sounding rocket/launch vehicle

分类

航空航天

引用本文复制引用

叶定友,张德雄..中国航天固体火箭技术的发展[J].固体火箭技术,2002,25(2):1-7,7.

固体火箭技术

OA北大核心CSCDCSTPCD

1006-2793

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