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- Using pintle technology, a conventional solid propellant rocket motor can provide variable thrust levels, increasing the energy utilizing efficiency and improving the capability of the missile. 喉栓式变推力发动机可实现固体火箭发动机的推力调节，提高能量利用效率，从多方面提升导弹武器的作战效能，因此具有强烈的军事需求。
- J.J. Choury,carbon/carbon materials for nozzle of solid propellant rocket motors[J].AIAA76-609. 崔红;李瑞珍;苏君明等.;多元基体抗烧蚀炭/炭复合材料的微观结构分析[J]
- The results of the experiments show that the technique is a rapid, effective method for the disbond detecting of solid propellant rocket motors. 实验研究结果表明,该技术可对固体火箭发动机钢筒与绝热层之间的脱粘作快速有效的检测。
- internal ballistics of solid propellant rocket motor 固体火箭发动机内弹道学
- SOFTWARE MODEL AND THE REALIZATION OF AUTOMATIC PARAMETER DESIGN OF A SOLID PROPELLANT ROCKET MOTOR 固体火箭发动机自动化参数设计软件模型与实现
- THE DYNAMIC COMBUSTION RATE CHARACTERISTICS OF SOLID PROPELLANT ROCKET MOTOR WITH HIGH SPEED ROTATING 高速旋转固体火箭发动机的动态燃速特性研究
- Contour design and numerical calculation of certain solid propellant rocket motor nozzle 某型号固体火箭发动机喷管型面设计与数值计算
- Dynamic Characteristics Analysis of Solid Propellant Rocket Motor Thrust Vector Control System 固体火箭发动机推力向量控制系统动态性能分析
- solid propellant rocket motor 固体火箭发动机
- Infrared Thermal Wave NDT on the Disbonds of the Heat Insulated Layer in Solid Propellant Rocket Motors 固体火箭发动机绝热层脱粘的红外热波无损检测
- We shall try by means of a highly simplified development to expose certain advantages and disadvantages of solid propellant rocket systems. 我们想通过相当简单的推导来试图阐明固体推进剂火箭系统的某些优缺点。
- According to the requirement of pasty propellant rocket motor, a composite plasma igniting plan was adopted. 摘要根据膏体推进剂火箭发动机。
- Solid propellant rocket motors 固体火箭发动机
- This pa per presents plume temperature measurements of a mounted solid propellant rocket engine measured using a 6-target 8-wavelength pyrometer. 对于固体火箭发动机羽焰温度的测量是困难的,了解其温度分布对于研究发动机内燃烧流场的特性有重要价值。
- Solid Propellant Augmented Rocket Motor 固体推进剂改进助推火箭发动机
- Solid propellant ramjet rocket motor 固体火箭冲压发动机
- SPRINT (Solid Propellant Rocket Intercept Missile) 固体推进火箭截击导弹
- unguided solid propellant rocket 无控固体推进剂火箭
- Solid Propellant Rocket Intercept 固体推进剂火箭拦截
- A CAD System for Solid Propel? Lant Ramjet Rocket Motor 固体火箭冲压发动机一体化CAD系统设计
