上海航天2012，Vol.29Issue(4)：41-48,8.
低温推进剂火箭发动机预冷方案研究
Research on Precooling of Cryogenic Propellant Rocket Engines
孙礼杰 1樊宏湍 2刘增光 2张亮1
作者信息
- 1. 上海宇航系统工程研究所,上海201108
- 2. 上海航天技术研究院,上海201109
- 折叠
摘要
Abstract
The bleed, natural recirculation and forced recirculation preeooling methods used in cryogenic propellant rocket engine in domestic and aboard were summarized in this paper. The research on the precooling of new cryogenic propellant rocket engine for the new generation launch vehicle in China was introduced. The key factors of propellant type, the sub-stage of the engine and multifactor integrated of natural recirculation which affected the precooling scheme, and the key technologies such as the maintaining and boiling heat transfer and two- phase flow numerical simulation were discussed.关键词
运载火箭/低温推进剂/发动机预冷/排放预冷/自然循环预冷/强制循环预冷Key words
Launch vehicle/Cryogenic propellant/Engine precooling/Bleed precooling/Natural recirculationprecooling/Forced recirculation precooling引用本文复制引用
孙礼杰,樊宏湍,刘增光,张亮..低温推进剂火箭发动机预冷方案研究[J].上海航天,2012,29(4):41-48,8.
