1.
Numerical Simulation of Combustion Instability of a LOX/GH_2 Rocket Engine
氢氧火箭发动机不稳定燃烧数值研究
2.
The effect of initial hydrogen temperature on LOX/GH_2 liquid rocket engine combustion instability
氢喷射温度对氢氧火箭发动机燃烧稳定性的影响
3.
The rocket engine carries with it the oxygen of its own .
火箭发动机自带氧气。
4.
Low frequency characteristics analysis of LOX / kerosene staged combustion cycle rocket engine
液氧/煤油补燃火箭发动机氧路低频动特性分析
5.
When a rocket travels in space, its engine goes on working, because the rocket carries oxygen with it.
火箭在太空中运行时，发动机不停地工作着，因为火箭本身带着氧气。
6.
Investigation of GO_2/kerosene thrust chamber of the main rocket engine for the RBCC propulsion system
RBCC推进系统主火箭发动机气氧/煤油推力室研究
7.
Nonlinear Dynamic Stability of Liquid Hydrogen Turbopump Rotor-S eal System in Rocket Engine
火箭发动机液氢涡轮泵转子-密封系统的非线性动力稳定性
8.
solar heating rocket engine
太阳加热式火箭发动机
9.
turbo-ram rocket engine
涡轮冲压式火箭发动机
10.
nuclear engine for rocket vehicle application
火箭飞行泼核发动机
11.
assist-climb rocket engine
爬升助推火箭发动机
12.
hybrid propellant rocket engine
混合推进剂火箭发动机
13.
air-breathing rocket engine
空气喷气火箭发动机
14.
dual thrust rocket engine
双级推力火箭发动机
15.
Cycle Power Balance Analysis for Liquid Rocket Engine with LO_2/RP-1 Propellant Combination
液氧/煤油推进剂液体火箭发动机循环动力平衡分析
16.
These were rockets with more than one engine.
多级火箭是装有一台以上发动机的火箭。
17.
The liquids employed for rocket propulsion are called propergols.
用于火箭发动机的液体称为液体火箭推进剂。
18.
Influence of mass flux of oxidizer on regression rate of solid fuel in hybrid rocket motors
氧化剂质量通量对固液火箭发动机中固体燃料退移速率的影响