1) liquid-oxygen motor
液氧火箭发动机<火>
2) 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
3) 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
4) LOX /kerosene rocket engine
液氧/煤油火箭发动机
1.
The procedure of the throttle valve core contour optimized design for LOX /kerosene rocket engine was described in this paper.
简要叙述了液氧/煤油火箭发动机节流阀阀芯型面优化设计的方法。
5) hybrid rocket
固液火箭发动机
1.
In order to know combustion process of hybrid rocket,pyrolysis test of solid fuel was carried out by using hot-plate heat conduction mode,then chemical kinetic parameters of solid fuel were obtained.
为了认清固液火箭发动机混合燃烧过程,采用热平板导热方式对固体燃料进行热分解实验,得到了固体燃料的化学动力学参数。
2.
Remarkable advantage such as low costing, high security, high reliability, low exhaust plume signal characteristic and environment non-pollution, which does not belong to Solid Rocket Motor (SRM) or Liquid Rocket Engine (LRE), advances astronautic experts to have much more interest in Hybrid Rocket Motor (HRM).
固液火箭发动机在成本控制、安全性、可靠性，排气羽流信号特征、环境等方面的优良特性，越来越受到国内外航天专家的重视。
6) hybrid rocket motor
固液火箭发动机
1.
Investigation on pyrolytic product distribution of low density polyethylene of hybrid rocket motor;
固液火箭发动机燃料LDPE热解产物分布研究
2.
Effects of combustion chamber structure on combustion and flow of hybrid rocket motor;
燃烧室结构对固液火箭发动机燃烧与流动的影响研究
3.
Research on Working Process of the 85% H_2O_2-PE Hybrid Rocket Motor;
85%H_2O_2-PE固液火箭发动机工作过程研究
补充资料：固－液火箭发动机
见导弹推进系统。
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