盈余从美国s。空军固体火箭马达。
本文介绍一种设计固体火箭喷管的新方法。
A new method of the solid propellant rocket nozzle design is presented.
固体火箭发动机设计是一项复杂的系统工程。
Solid rocket motor design is a complicated systems engineering.
据说，这种东西最早是由NASA作为固体火箭燃料而研发的。
Supposedly, it was developed by NASA as a solid rocket fuel.
作为一个例子，计算了一个固体火箭发动机壳体的强度。
As an example, the strength of a solid fuel rocket engine shell is calculated.
介绍了一种固体火箭发动机试验数据分析处理及管理系统。
A software system for solid rocket motor test data analysis and management is introduced.
对固体火箭助推器进行了较详细的分析，证明方案是可行的。
On the basis of more detailed analysis, verified is that the idea is very feasible.
此项设计技术对带反向喷管的固体火箭发动机设计具有参考作用。
This technique is available for the design of SRM with reverse nozzle.
该项研究为长时间工作固体火箭发动机燃烧室热防护层设计提供了有效的分析手段。
This research can offer an effective analytical method for long-time working solid rocket motors.
闪闪发亮的白色战神i - X的核心是一个巨型固体燃料火箭推进器。
The gleaming white Ares I-X, at its core, is a giant solid rocket booster.
对大型运载火箭的固体助推器，通常采用摆动喷管推力向量控制。
The deflecting nozzle thrust vector control is usually used in a large solid booster.
对大型运载火箭的固体助推器，通常采用摆动喷管推力向量控制。
The deflecting nozzle thrust vector control is usually used in a large solid booster.
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