SRM的例句大全

A new seal structure suited to solid rocket motors ( SRM) is introduced, and threaded joint structures and sealing glue compound are studied.

提出了一种适用于固体火箭发动机（SRM）的新型密封结构，并对应用于特定尺寸的螺纹联接结构方式、胶种选择进行了研究。

Based on pressure and high low temperature cycling tests and theoretic analysis, the threaded joint parts filled with sealing glue compound show excellent seal ability, and can be applied to SRM.

通过压力、高低温循环等大量的试验和理论分析表明：采用填充密封胶的螺纹联接密封结构具有优异的密封性，适宜在固体火箭发动机环境中应用。

Selection and Orifice Diameter Calculation for Safety Valve IDENTIFICATION OF THROAT RADIUS VARIATION FOR SRM

安全阀的选用及喉径计算

The Implementation of Gain-scheduling Control on SRM with DSP

用DSP实现开关磁阻电机的增益调度控制

The characteristic velocity, area of nozzle throat and other parameters are calculated by using the static test results of solid rocket motor ( SRM) and introducing generalized pressure coefficient and thrust coefficient.

利用发动机地面试验结果，引入广义的压强系数和推力系数，计算了发动机的特征速度、喷管喉部面积等参数。

The analysis of interior ballistic dispersion of SRM during thrust termination with Monte Carlo method

用Monte Carlo法分析固体火箭发动机推力终止过程内弹道散布

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。

Analysis and calculation for correction of instantaneous vacuum thrust in simulated altitude test of SRM

固体发动机高空模拟试验瞬时真空推力的修正分析与计算

In this paper, determination of potassium ( K) in milk powder standard reference material ( SRM) by IDMS was described. The result of the determination corresponded with the certified value of milk powder SRM.

本文叙述了用IDMS法测定奶粉标准物质中钾含量的方法，本方法测得值与原定值结果相符。

On the basis of analyzing SRM throat thermal ambient and ablative action of C/ C composites, factors affecting ablative performance of C/ C composites are discussed from the viewpoint of material property.

在分析固体火箭发动机喷管喉衬热环境与碳/碳复合材料烧蚀行为的基础上，从材料的角度讨论了影响碳/碳复合材料烧蚀性能的因素。

Engineering calculation for erosion and thermal structure of throat-insert of a SRM nozzle

发动机喷管喉衬烧蚀及热结构工程计算

HASP SRM fully aligns with the software product lifecycle. HASPSRM

完全遵循软件产品的生命周期。

Effects of control flow parameters on vortex valve SRM thrust modulation

控制流参数对涡流阀变推力固体发动机性能的影响

Switched Reluctance Motor ( SRM) system has the advantages of simple structure, rugged, low cost, high reliability, high efficiency and good speed performance.

开关磁阻电机控制系统具有结构简单、坚固耐用、成本低廉、工作可靠性高、运行效率高、调速性能好等优点。

Research of analysis method for storage life of SRM

舰上导弹固体火箭发动机贮存寿命的分析方法研究

Analysis of Second Gas Injection Affecting Factor on SRM Thrust Vector Control

气体二次喷射SRM推力矢量控制影响因素分析

The software requirement management ( SRM) is the first key process area ( KPA) in the CMM.

需求管理是CMM中的首个关键过程域。

Study on Canted Scarfed Flow-backward Multi-nozzle SRM; Calculation Method of Bevel Angle in Vent Pipe

小型斜置倒流多喷管固体火箭发动机研究排汽管斜切口出流偏转角的计算方法

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

Experimental investigation of erosion performance of pintle in thrust-controllable SRM Influence of phase change of dispersed-phase particle in SRM chamber on throat insert erosion

变推力固体火箭发动机喉栓烧蚀试验研究固体发动机燃烧室离散相颗粒相变对喉衬烧蚀的影响