The Ares I-X is not a full Ares I rocket. Its first stage is a four-segment solid rocket booster ?

“战神I-X”并非完整的“战神I”火箭，它的第一级包含4段固体火箭助推器和第5段没有推进作用的模型部分。

A solid rocket cannot be throttled , either—once lit, it runs until the fuel is expended.

此外，固体火箭也不能够调节燃料，一旦点燃了，就会运作到燃料用尽为止。

Using solid rocket gas generator, sea level static ejector mode experiment was conducted.

利用固体火箭发动机做为燃气发生器, 成功地进行了海平面静态自由引射实验.

Investigated charring erosive characters of internal insulation of solid rocket motor under flight acceleration.

研究了固体火箭发动机内绝热层在飞行加速度条件下的炭化烧蚀特性.

The present situation and development of solid rocket motor liner forming at home are reviewed. The test results of novel solvent-free high solid content liner adopting throw…

综述我国固体火箭发动机衬层成型工艺的现状和发展，介绍了无溶剂高固体份衬层抛涂成型新技术的试验结果。

Introduced the Method of electronic optical data high speed acquisition of ultraviolet radiation of solid rocket plume.

详述了固体火箭羽烟紫外辐射的光电高速采集方法，并实时对导弹逼近告警。

A response surface method ( RSM ) for structure reliability analysis of solid rocket motor ( SRM ) grain was presented.

发展了一种固体火箭发动机药柱结构可靠度分析的响应面法.

The part's design tolerance, the processing tolerance and the assembling tolerance can cause thrust misalignment of solid rocket.

零部件的设计公差、加工误差和装配误差会使固体火箭发动机产生推力偏心。

Based on the progress of nondestructive testing technology of solid rocket motor, the prospect of developing technology in the area was pointed out.

在回顾固体火箭发动机无损检测技术发展的基础上，展望了该研究领域未来的发展趋势。

The causation of some defects and its effects on solid rocket motor were analyzed, the latest nondestructive testing methods of motor were also introduced.

分析了固体火箭发动机燃烧室各种缺陷的形成原因及其对发动机的影响，介绍了目前用于发动机无损检测的几种方法。