reverse thrust的例句大全

The structural space of thrust termination mechanism in the solid motor is very limited. In order to meet the demand that negative thrust of the motor is not less than zero, efficiency of reverse thrust must be improved as far as possible.

某固体发动机推力终止装置结构空间十分有限，为保证推力终止时发动机负推力大于等于零的要求，必须尽可能地提高反推力效率。

Fault strikes mostly include two direction: northeast faults, e.g.Thirteen Mound-Xiazhuang reverse thrust;

该地区主要发育两个方向的断裂：北东向的十三陵-下庄逆冲推覆构造等；

Living things throve in Devonian strata of the nappe, and their species were numerous. APPLICATION OF ROTARY PERCUSSION DRILLING TECHNOLOGY IN REVERSE THRUST NAPPE STRUCTURE FORMATION

旋冲钻井技术在逆掩推覆体地层的应用

Study on the Reverse Thrust of Water Jet Through Conical Nozzles

锥形喷嘴水射流反推力的研究

In this paper, a simple method for analysis of ground test data of the solid rocket motor with reversal nozzles is presented based on solving the reverse thrust at an altitude from ground test data.

文中介绍了根据地面实验数据分析反喷管在高空提供的反推力，为带反喷管发动机地面实验数据处理提供了简便的分析方法。

Depending on the seismic reflection surveys data, the reverse faults on the front of the nappe in Kalpin thrust tectonic zone form an integrate detachment surface in the deep along the gypsum stratum in Cambrian.

地震勘探资料显示，各褶皱带前缘活动逆断裂在深部归并于统一的、由寒武系中的石膏层组成的滑脱面。

When the dip angle is shallow a reverse fault is often described as a thrust fault.

倾角较小的逆断层常称为逆冲断层.

Utilizing the piezoelectric force-measuring platform together with its developed test software, the thrust vector of space solved by reverse method, the excursion of the thrust vector and thrust misalignment angle are obtained.

利用设计的压电式测力平台和其相应的测试软件以及测试系统，用反求法求得空间力矢量大小、推力矢量的推力偏移量、推力偏斜角。

Measuring method of opening time and operating synchronism of the reverse nozzle closures of solid rocket motor during thrust termination test was studied.

研究了固体火箭发动机推力终止试验时，反向喷管堵盖打开时间及同步性测量方法。

As the transient parameters during thrust termination of SRM with four reverse nozzles are determined by identification techniques and considered as random variables which obey normal distribution, the interior ballistic dispersion during thrust termination can be analyzed by Monte Carlo method.

用辨识方法确定了带反喷固体火箭发动机推力终止过程中的瞬变参数，视这些参数是服从正态分布的随机变量，用Monte Carlo方法分析了推力终止过程内弹道的散布。

Reverse JATO jet thrust reverser

喷气发动机推力反向器