1) Hydrogen oxygen engine
氢氧发动机
1.
Following a brief analysis of the characteristics of several kinds of power cycles,the discussion is emphasized on the cryogenic technique of the high pressure closed cycle hydrogen oxygen engine.
简要分析几种不同动力循环的特点， 重点介绍大推力、高性能氢氧发动机采用补燃动力循环进行的研究及高压补燃氢氧发动机中的低温技
2) hydrogen peroxide engine
过氧化氢发动机
1.
Considering the low-frequency oscillation phenomenon which occurs in experiment of hydrogen peroxide engine,simulation and analysis of the phenomenon based on the propulsion system models were made,and a stable engine was achieved.
针对过氧化氢发动机试验中出现的低频振荡现象,通过建立发动机系统模型,对这种振荡现象进行了仿真和分析,成功实现了发动机的稳定工作。
3) LH_2/LOX rocket engines
液氢液氧发动机
5) hydrogen/oxygen liquid propellant rocket engine
氢/氧液体火箭发动机
1.
Mass analysis of pump-pressurized hydrogen/oxygen liquid propellant rocket engine;
泵压式氢/氧液体火箭发动机质量分析
6) LH_2/LOX rocket engine
液氢液氧火箭发动机
1.
Non-linear static charactersitic simulation and analysis for large LH_2/LOX rocket engine;
液氢液氧火箭发动机非线性静态特性仿真与分析
补充资料：航空发动机推重比(见航空发动机推力)
航空发动机推重比(见航空发动机推力)
thrust to weight ratio of aeroengine
hQngkong角dong)1 tuizhongbi航空发动机推重比〔thros*:。wdgh:ra-tio of aeroengine)见航空发动机推力。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条