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- 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 Rocket Engine Modal Test and Analysis Technique 固体火箭发动机试验模态分析技术研究
- Defect-detecting equipment for solid propellant rocket engine 固体火箭发动机探伤设备
- Structural Integrity Analysis for Solid Propellant Rocket Engine under Overload 过载条件下固体发动机药柱结构完整性分析
- Photoelastic Analysis of Combustion Chamber of Solid Propellant Rocket Engine 固体火箭发动机燃烧室光弹性分析
- EFFECTS OF AI_20_3 DEPOSIT ON PERFORMANCE OF SOLID PROPELLANT ROCKET ENGINE Al_2O_3沉积对发动机推力的影响
- THE PREDICTION OF THE SPECIFIC IMPULSE FOR SOLID PROPELLANT ROCKET ENGINE BASED ON ARTIFICIAL NEURAL NETWORK 基于神经网络的固体火箭发动机比冲性能的预示研究
- Plume temperature measurement of a solid propellant rocket engine using multispectral thermometry 基于多光谱法的固体火箭发动机羽焰温度测量
- A Study on Measurement Method of Exhaust Flames Temperature for Solid Propellant Rocket Engine 固体火箭发动机羽焰测温方法研究
- Research on Genetic Algorithm for Plume Temperature of Solid Propellant Rocket Engine 固体推进剂火箭发动机羽焰温度诊断的遗传算法研究
- RESEARCH ON THE DATA PROCESSING METHOD OF SOLID PROPELLANT ROCKET ENGINE PLUME TEMPERATURE 一种测量固体火箭发动机羽焰温度的数据处理方法研究
- solid propellant rocket engine plume temperature multispectral thermometry true temperature emissivity. 标 签 固体火箭发动机 羽焰温度 多光谱测温 真温 发射率.
- solid propellant rocket engine 固体推进剂火箭发动机
- 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。
- 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]
- It is an important and basic issue to choose monitoring parameters of Liquid propellant Rocket Engine (LRE) monitoring system in ground test. 摘要确定监测参数是液体火箭发动机地面试验监控系统的一个重要而基础的问题。
- 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。
- The compound solid propellant used by rocket engine is made of adhesive, oxidizer and some other additives.All of those are casted or extruded then solidified to form the propellant. 火箭发动机所使用的复合固体推进剂，是利用胶粘剂、氧化剂和其它添加剂等成分经浇注或挤出后，固化而成的固体药柱。
- The principle of coriolis force mass flowmeter and its application in gelled propellant rocket engine test are introduced,results of the test are also analyzed. 介绍了科氏力质量流量计的原理及其在凝胶发动机试车中的应用,并对热试车的测量数据进行了分析。
- 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。
