摘要
阐述了涡轮泵的技术发展水平在液体火箭发动机研制中的重要地位;分级燃烧循环系统发动机涡轮泵的设计特色;苏联涡轮泵总体设计的特点;并对预压泵、轴向力平衡活塞、两相流诱导轮、正反旋涡轮等涡轮泵新技术的设计原理进行了概述.
The following contents are discussed in the paper, the essential position of turbopump technology in liquid rocket engine development,the design charateristics of turbopump for stage-combustion engines,and the general assembling design features of turbopumps in USSR.In addition,an overview on the design principles of turbopump technology-booster pumps,axial load balancing pistons,two-phase flow inducers,and counter-rotating turbines are also discussed
出处
《推进技术》
EI
CAS
CSCD
北大核心
1991年第6期23-30,68,共9页
Journal of Propulsion Technology
关键词
液体推进剂
火箭发动机
涡轮泵
Liquid propellant rocket engine,Rocket fuel system,Review
