说明:双击或选中下面任意单词,将显示该词的音标、读音、翻译等;选中中文或多个词,将显示翻译。
您的位置:首页 -> 句库 -> 固体火箭推进
1.
The Analysis and Numeration of Solid Rocket Propellant's Finite Element Theory;
固体火箭推进剂有限元理论分析与计算
2.
The Real Time and in Situ Infrared Characteristics Measurement of Plume of Solid Rocket Propellant by Remote Sensing FTIR;
遥感FTIR光谱实时原位测定固体火箭推进剂羽流红外特性
3.
Virtual Machine Tool Technology for Solid Rocket Propellant
用于固体火箭推进剂的多功能集成虚拟机床技术
4.
The calculation of the intrinsic frequency of the liquid rocket propulsion system
液体火箭推进系统液路固有频率计算
5.
solid Rocket Booster
固体燃料火箭助推器
6.
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。
7.
redesigned solid rocket booster (RSRB)
重新设计的固体燃料火箭助推器
8.
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
9.
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)
10.
Study on General Calculation of Natural Frequency for Liquid Engine Flow System in Launch Vehicle
液体运载火箭推进系统固有频率的通用化计算研究
11.
bipropellant liquid rocket motor
二元推进剂液体火箭发动机
12.
bipropellant rocket
双元液体推进剂火箭发动机
13.
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
14.
We shall try by means of a highly simplified development to expose certain advantages and disadvantages of solid propellant rocket systems.
我们想通过相当简单的推导来试图阐明固体推进剂火箭系统的某些优缺点。
15.
A Study of the Synchronism of Double Solid Boosting Rockets Applied to UAV
无人机双发固体火箭助推器同步性研究
16.
The Solid Rocket-Ramjet Engine Thrust Calculation and Experimental Research of Connected-Pipe Testing;
固体火箭冲压发动机推力计算与实验研究
17.
Internal ballistic regulating property of variable thrust pintle SRM
喉栓式变推力固体火箭发动机内弹道调节特性
18.
Experimental investigation of erosion performance of pintle in thrust-controllable SRM
变推力固体火箭发动机喉栓烧蚀试验研究