低温火箭

新型低温火箭发动机超临界燃烧研究进展

Research and Development of Supercritical Combustion in Cryogenic Rocket Engines

密度测量在低温液体火箭发动机试验中的作用

The Effect of Density Measurement in Cryogenic Liquid Rocket Engine Test

低温推进剂火箭发动机循环预冷试验研究

The Experiment Study of Circulating Chilldown of Cryogenic Rocket Engine

在低温液体火箭发动机的试验中，对液体密度的测量是很重要的。

It is very important to measure liquid density in cryogenic liquid rocket engine test .

低温液体火箭发动机模拟预冷过程的传热与压降

Heat transfer and pressure drop during the modeling precooling test of a cryogenic liquid rocket engine

低温推进剂火箭发动机泵出口密度、温度计算的一种新方法

A novel method of calculating the density and temperature of cryogenic propellant rocket engine pump exit

以液氮为工质，进行了低温推进剂火箭发动机循环预冷的试验研究。

A series of experiments are made to study circulating chilldown of cryogenic rocket engine . The working fluid is liquid nitrogen .

本文首先介绍了低温推进剂火箭发动机的各种预冷方法的研究和应用的历史和现状，然后重点对自然循环预冷法进行了实验研究。

The paper firstly reviews the history and developments of the research and application on kinds of precooling methods recently adopted . Then , the paper lays emphasis on the experimental investigation of natural circulation precooling .

低温推进剂液体火箭发动机超导电磁泵压循环系统初步设想

Conceive of Cryogenic Propellant Engine Superconductor Electromagnetic Pump Circulating System

低温技术在氢氧火箭发动机试车台上的应用

The Application of Cryogenic Technology in LOX / LH 2 Rocket Engine Test Stand