1.
bipropellant rocket
双元液体推进剂火箭发动机
2.
To appreciate the unsteady environment existing in liquid propellant rocket chambers it is necessary that the steady state be well understood.
为了分析液体推进剂火箭发动机燃烧室中存在的非稳态环境，必须很好地了解稳态状态。
3.
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。
4.
bipropellant liquid rocket motor
二元推进剂液体火箭发动机
5.
The Research on Influence of Low Freezing Point Propellant on Performance of Liquid-propellant Rocket Engine
低冰点推进剂对液体火箭发动机性能影响研究
6.
hybrid propellant rocket engine
混合推进剂火箭发动机
7.
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
8.
Research on Working Process of Pasty Propellant Rocket Motor
膏体推进剂火箭发动机工作过程研究
9.
The Study on Mutilple Starts of Pasty Propellant Rocket
膏体推进剂火箭发动机多次启动技术研究
10.
Thermodynamic cycle analysis on solid propellant air-turbo-rocket
固体推进剂吸气式涡轮火箭发动机的气动热力循环分析(英文)
11.
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
12.
Analysis and Control of the Structural and Damage Madel of Thrust Chamber Inliquid Propellant Rocket Engine;
液体火箭发动机推力室结构损伤分析和控制
13.
The Mechanism and Pharmacological Prevention of Acute Lung Injury Induced by Inhalation of Liquid Rocket Propellant;
大剂量火箭液体推进剂吸入引起的急性肺损伤—发生机制及药物防治研究
14.
forward force produced by a propeller,jet engine,rocket,etc
（推进器、喷气发动机、火箭等的）推力.
15.
Progress in combustion characteristic research of liquid rocket gelled propellants
液体火箭凝胶推进剂燃烧特性研究进展
16.
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
17.
It is reasonable that this result should be generally applicable also to liquid-propellant rockets.
这个结果通常也应适用于液体推进剂火箭。
18.
Rocket motors have many advantages over other forms of propulsion.
火箭发动机比其他推进器有许多优点。