火箭发动机

As a result, a Pyrogen Igniter , which is essentially a small rocket motor, was developed.

因此，一个热原点火器，这基本上是一种小型火箭发动机，开发。

An innovative igniter based on catalytic decomposition of N2O was designed and manufactured.

利用N2O催化分解原理，设计了一个用于启动N2O混合火箭发动机的催化点火器。

Finite element method is used in the study of nozzle damping of instable combustion in a solid rocket motor.

应用有限单元法研究固体火箭发动机不稳定燃烧中的喷管阻尼，并用波衰减对比法进行了试验研究。

The colouring agent makes it possible to inspect the shellingout quality of the adhesive. Adhesive ZJ-3101 is of great originalbonding power, and its performance is reliable and stable. It has passed the engine test.The performance test indicates that adhesive ZJ-3101 has great power to bind NBR insulant to s...

ZJ-3101胶初粘性能好，产品性能稳定可靠，试验结果表明：ZJ-3101粘接剂对于固体火箭发动机钢壳体(30CrMnSiA钢、D6AE钢、钛合金)、以及铝镁合金或玻璃钢材质与丁腈橡胶绝热层的粘接均有良好的效果。

The simulation results of liquid propellant rocket engine demonstrate that modal interval analysis is effective to complex dynamic systems.

通过对某泵压式液体火箭发动机稳态工作过程的模态区间仿真计算，证明模态区间分析方法对复杂动态系统建模仿真是有效的。

The experiments indicate that the method making the solid rocket motor as plasma ionizer is effective,and the required electron density value can be gained.

试验表明，将固体火箭发动机作为等离子体发生器是一种行之有效的方法，可以获得需要的电子密度值。

Results of the research can be applied to health monitoring of liquid propellant rocket engine in ground test.

本论文的研究成果已经可以用于液体火箭发动机地面试车的故障检测。

The development approaches of various types of liquid propellant rocket engines are discussed.

对各种型式的液体火箭发动机的发展途径进行讨论。

The conclusions in this paper are for refference in the design calculation of the liquid propellant rocket engines.

本文所得的结果，对液体火箭发动机设计计算有一定的参考价值。

It is an important and basic issue to choose monitoring parameters of Liquid propellant Rocket Engine monitoring system in ground test.

确定监测参数是液体火箭发动机地面试验监控系统的一个重要而基础的问题。

But we don't care about Battlegrounds.

但我们并不在乎沙场中的显露。

Ah! don't mention it, the butcher's shop is a horror.

啊！不用提了。提到肉，真是糟透了。