Four nozzles , canted outboard, split the exhaust of the solid rocket motor into four equal tails.

四个向外倾斜的喷管把固体火箭发动机的排气流分成四个相等的尾巴.

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Rocket motor cases and the specially designed production equipment therefor.

四、火箭发动机的壳体及为其专门设计的生产设备.

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Solid propellant is fuel and core part of solid rocket motor.

固体推进剂是固体火箭发动机的燃料,为其核心部分.

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Computational result of free - efflux field for one rocket motor has been presented.

格式及流动求解的组合格式,给出了某火箭燃气自由射流流场的计算结果.

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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.

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The influence of structure axial vibration on the internal ballistics of solid rocket motor was investigated.

文中研究了固体发动机结构的轴向振动对燃烧室内弹道性能的影响.

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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.

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Extend - range solid propellant rocket motor is an important part of the hybrid base - burner - rocket extending range shell.

增程固体火箭发动机是底排 — 火箭复合增程炮弹的主要部件之一.

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A rocket motor's'bullets'are minute, high - speed particles produced by burning propellants in a suitable chamber.

火箭发动机的作用是瞬间的, 在适当的地方燃烧推进物生成 高速 粒子.

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The experiment result can use to internal insulation design of solid rocket motor.

实验结果可作为发动机绝热层设计的依据.

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High speed rotation affects the performance of solid propellant rocket motor.

在高速旋转条件下,固体火箭发动机的工作性能将受很大影响.

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