solid rocket的例句大全

A method of acoustic analysis and predication of the combustion stability for solid rocket motors

固体火箭发动机的声学分析及燃烧稳定性预估

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The Test of Dynamic Balance for Perigee Kick Solid Rocket Motor

近地点变轨固体火箭发动机动平衡试验

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Development of Space Solid Rocket Motors in China

中国空间用固体火箭发动机的发展

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Allan J.McDonald, "Design evolution of the space shuttle solid rocket motors"

航天飞机固体火箭发动机的设计演变

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Influence of ambient temperature on solid rocket motor airtight test

环境温度对固体火箭发动机气密性检查影响分析

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Numerical analysis of grain large deformation for solid rocket motor

固体火箭发动机药柱大变形数值分析

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Effects of Solid Rocket Motor Material Properties on the Structure Integrity

材料性能对固体发动机结构完整性的影响

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The Structure Integrity Analysis of Free Loading Solid Rocket Grains

自由装填药柱的结构完整性分析

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The structure integrity analysis of solid rocket motor grain with cohesive cavity

含内聚空洞的固体发动机药柱结构完整性分析

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Health monitoring of solid rocket structure based on fiber grating sensing

基于FBG传感器的固体火箭发动机结构健康监测技术

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Rotating acceleration has inevitable influence on the work process of Solid Rocket Motor: flow of combustion chamber and nozzle is changed; the pressure, mass flow rate and the specific impulse of Solid Rocket Motor are affected by the spinning.

旋转产生的加速度必然对固体火箭发动机的工作过程产生影响：使燃烧室和喷管中的燃气流动发生变化，对燃烧室工作压力质量流率及冲量产生影响。

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Graph Morphing applied in design optimization for solid rocket motor

图形变形法在固体火箭发动机设计优化中的应用

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Design optimization for solid rocket motor based on graph morphing

基于图形变形法的固体火箭发动机优化设计

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The feasibility of applying fiber gratings sensing on health monitoring of solid rocket motor ( SRM) is discussed, including the strain measurement, temperature measurement and damage measurement.

讨论光纤布拉格光栅（FBG）传感技术用于固体火箭发动机结构应变场、温度场和损伤状况健康监测的可行性。

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Using pressure-controlled T-burner the anthors have determined the pressure coupling responses of three smokeless solid propellants. From the experiment results we have believed that the combustion catalyst may play an important role in eliminating the combustion instability in a solid rocket motor.

用压力可控T形燃烧器测量了三种无烟推进剂压力耦合响应函数，总结到一些实验规律，提出燃烧催化剂对抑制不稳定燃烧可能起到的重要作用。

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The erosive property and principle of copper-infiltrated graphite as solid rocket motor ( SRM) throat insert and tailpipe nozzle bushing are presented.

介绍了石墨渗铜材料作为固体火箭发动机（SRM）喉衬与长尾管衬套的烧蚀特性和机理。

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cold gas simulation on aft-end internal flow for solid rocket motor with submerged nozzle

含潜入喷管发动机尾部流场冷流模拟

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design method for aft-end igniter of small-scale solid rocket motor

小型固体火箭发动机尾部点火器设计方法

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unsteady numerical simulation of controllable thrust solid rocket motor

可控推力发动机非稳态数值模拟

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the shuttle orbiter is visible on the image right, attached to a brown liquid fuel tank and two white solid rocket boosters .

在影像右侧可以看到航天飞机，它连接着一个灰色的液体燃料箱以及两枚白色的固体火箭推进器。

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