1.
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
2.
ADVANCED MODEL OF STATIC CHARACTERISTIC FOR LIQUID OXYGEN/KEROSENE
液氧/煤油高压补燃火箭发动机非线性稳态模型——考虑推进剂温升与密度变化
3.
Study on start-up of the staged combustion LOX/kerosene rocket engine
液氧/煤油补燃循环发动机起动过程研究
4.
Research on the low frequency characteristics of LOX/kerosene staged combustion cycle engine
液氧/煤油补燃发动机低频频率特性研究
5.
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
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.
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
8.
The Research on Characteristic Performance of Combustion Flow Field in Secondary Combustion Chamber for Extended Range Solid Rocket Ramjet
增程固体火箭冲压发动机补燃室燃烧特性研究
9.
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
10.
Techniques of kerosene booster turbopump for LOX/kerosene staged combustion cycle engine
液氧/煤油发动机煤油预压涡轮泵技术
11.
An Innovative Partition Model of Liquid Rocket Engine Combustion Chambers
液体火箭发动机燃烧室的一种分区模型
12.
Numerical Simulation of Working Process of Combustion in Hybrid Rocket Motor;
固液火箭发动机燃烧室工作过程数值模拟
13.
The rocket engine carries with it the oxygen of its own .
火箭发动机自带氧气。
14.
Effects of Jet Rotational Angle on the Second Combustor of Boron-based Propellant Solid Rocket Ramjets
含硼固体火箭冲压发动机中燃气旋流角对补燃室的影响
15.
High and low temperature test technology of kerosene of the LOX/kerosene engine
液氧/煤油发动机煤油高低温试验工艺技术
16.
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。
17.
Research on the Secondary Combustion Chamber Operation Process of Boron-Based Propellant Ducted Rockets;
含硼推进剂固体火箭冲压发动机补燃室工作过程研究
18.
Three-Dimensional Numerical Simulation of Afterburner Flow Field of Solid Rocket Ramjet
固体火箭冲压发动机补燃室流场三维数值计算研究