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Verification of RSRM Nozzle Thermal Models With ETM-3 Aft Exit Cone In-depth Temperature Measurements

机译:使用ETM-3尾部出口锥深度温度测量验证RSRM喷嘴热模型

摘要

One of the goals of the Engineering Test Motor (ETM-3) static test was to verify analytical models through the use of instrumentation that provide real-time transient temperature response of ablating phenolic liners. Accurate measurement of in-depth temperature is critical for validating the analytical models and assessing design safety margins for nozzle insulation materials. Recent developments of in-depth thermocouple plugs have been made to more accurately measure temperature response of nozzle Liners. Thermocouple plugs were installed at two axial stations (four plugs circumferentially at each station) near the end of the ETM-3 nozzle aft exit cone to gather temperature histories during and after motor operation. The thermocouple plugs were placed at depths that bounded the reusable solid rocket motor nominal measured char depth in order to portray the carbon phenolic temperature response during the charring process. The data were used to verify the analytical models during motor operation and to better define char penetration during heat soak after motor burn out.
机译:工程测试电机(ETM-3)静态测试的目标之一是通过使用仪器来验证分析模型,该仪器提供烧蚀酚醛衬里的实时瞬态温度响应。准确测量深度温度对于验证分析模型和评估喷嘴绝缘材料的设计安全裕度至关重要。深入的热电偶塞的最新发展已经可以更准确地测量喷嘴衬里的温度响应。热电偶塞安装在ETM-3喷嘴尾部出口锥末端附近的两个轴向位置(每个位置在圆周上有四个塞),以收集电动机运行期间和运行后的温度历史记录。将热电偶塞放置在限定可重复使用的固体火箭发动机标称测得焦深的深度处,以描绘在炭化过程中碳酚温度响应。数据用于验证电动机运行过程中的分析模型,并更好地定义电动机烧毁后的热浸过程中的炭渗透率。

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