这些元素甚至可以为火箭发动机提供燃料。
已完成的火箭发动机是如图2所示。
该火箭发动机和试验台是如图3所示。
介绍了国外固液火箭发动机研制的进展。
The development of hybrid rocket engine in abroad was introduced in this paper.
最后探讨了固液火箭发动机的应用范围。
At last, the applied category of the hybrid engines was discussed.
火箭发动机能在没有空气。的太空中工作。
电火箭发动机是一种新型的空间推进装置。
Electrical rocket engine is a new type of space propulsion system.
涡轮泵是液体火箭发动机的重要组成部份。
固体火箭发动机设计是一项复杂的系统工程。
Solid rocket motor design is a complicated systems engineering.
该火箭发动机成立，在试验台是如图3所示。
The rocket motor set up in the test rig is shown in Figure 3.
该火箭发动机成立，在试验台是如图2所示。
The rocket motor set up in the test rig is shown in Figure 2.
火箭发动机的泄漏是常见和极其危险的故障。
The leak of Liquid Rocket Engine (LRE) is very common and dangerous.
火箭发动机试验的立场，施加武力对负载细胞。
火箭发动机通常使飞行更快，但需要自携氧气。
A rocket engine typically goes faster but has to carry its own supply of oxygen.
然后将BP学习算法用于火箭发动机的故障诊断。
The BP algorithm is applied to rocket engine fault diagnosis.
这对提高火箭发动机壳体力学性能有很大的作用。
It can be very useful to promote the physical performance of rocket-engine-rind.
模型的8个火箭发动机，每个都有250磅的推力。
The model had eight working rocket engines with 250pounds of thrust each.
该机器可以有它自己的小型火箭发动机来定位和发动。
The craft may have its own small rocket engines for orienting and maneuvering.
作为一个例子，计算了一个固体火箭发动机壳体的强度。
As an example, the strength of a solid fuel rocket engine shell is calculated.
火箭发动机给汽车提供大量的动力，但是操作它只是开或关。
The rocket gives the car plenty of power, but it is either on or off.
介绍了一种固体火箭发动机试验数据分析处理及管理系统。
A software system for solid rocket motor test data analysis and management is introduced.
本文在大型压力水筒中研究了火箭发动机的水下分离特性。
The research on separation of underwater rocket flow in a large pressurized tank is presented.
在大约时速200英里时他将启动为火箭发动机传送htp的泵。
At about 200mph he will start the pump to deliver the HTP into the rocket.
在低温液体火箭发动机的试验中，对液体密度的测量是很重要的。
It is very important to measure liquid density in cryogenic liquid rocket engine test.
此项设计技术对带反向喷管的固体火箭发动机设计具有参考作用。
This technique is available for the design of SRM with reverse nozzle.
当前的可靠性增长管理方法在液体火箭发动机中的应用存在诸多问题。
There are still many problems using current reliability management method for liquid rocket engine.
酚醛树脂以其价格低廉、耐热性能优异，在火箭发动机上得到广泛应用。
Phenolic resins have been applied in rocket motor to offer high properties and low cost.
文中结合闭气装置工作环境，对火箭发动机的闭气装置性能进行了分析。
In this paper obturator performance of rocket engine is analyzed according to work environment.
文中结合闭气装置工作环境，对火箭发动机的闭气装置性能进行了分析。
In this paper obturator performance of rocket engine is analyzed according to work environment.
应用推荐