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A UNIQUE THERMOCOUPLE TO MEASURE THE TEMPERATURES OF SQUIBS, IGNITERS, PROPELLANTS AND ROCKET NOZZLES

机译:独特的热力计,可测量扁管,点火器,推进剂和火箭喷嘴的温度

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摘要

The temperatures produced by the various components in the propulsion system of rockets and missiles determine the performance of the rocket. Since these temperatures occur very rapidly and under extreme conditions, standard thermocouples fail before any meaningful temperatures are measured. This paper describes the features of a special family of high performance thermocouples, which can measure these transient temperatures with millisecond response times and under the most severe conditions of erosion. Examples of igniter, propellant and rocket nozzle temperatures are included in this paper. Also included is heat flux measurements made by these sensors in rocket applications.
机译:火箭和导弹推进系统中各个组件产生的温度决定了火箭的性能。由于这些温度非常迅速且在极端条件下发生,因此在测量任何有意义的温度之前,标准热电偶就会失效。本文介绍了一种特殊的高性能热电偶系列的功能,该系列可以在毫秒级的响应时间和最恶劣的腐蚀条件下测量这些瞬态温度。本文包括点火器,推进剂和火箭喷嘴温度的示例。这些传感器在火箭应用中进行的热通量测量也包括在内。

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