| 火箭发动机装药温度测量 |
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| 引用本文： | 郝巨东,尹宝明,周彦煌,王宏峰.火箭发动机装药温度测量[J].火力与指挥控制,2009,34(2). |
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| 作者姓名： | 郝巨东 尹宝明 周彦煌 王宏峰 |
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| 作者单位： | 1. 北方自动控制技术研究所,山西,太原,030006
2. 南京理工大学,江苏,南京,210094 |
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| 摘 要： | 随着火箭弹射击距离的不断增长,其发动机装药温度测量精度对落点精度的影响日益突出.提出了测量火箭弹装药代用材料的方法来测量火箭弹装药温度,克服了火箭弹装药温度测量困难,提高了测量精度.介绍了装药温度特性曲线测量方法,通过试验选取代用材料,设计了火箭弹装药相似体及药温测量装置,并对结果进行了分析.
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| 关 键 词： | 代用材料 装药温度测量 相似体 |
Measurement of Rocket Engine Charge Temperature |
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| HAO Ju-dong,YIN Bao-ming,ZHOU Yan-huang,WANG Hong-feng.Measurement of Rocket Engine Charge Temperature[J].Fire Control & Command Control,2009,34(2). |
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| Authors: | HAO Ju-dong YIN Bao-ming ZHOU Yan-huang WANG Hong-feng |
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| Institution: | 1.North Automatic Control Technology Institute;Taiyuan 030006;China;2.Nanjing University of Science and Technology;Nanjing 210094;China |
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| Abstract: | With the continuously increment of rocket projectile launching range,the influence from the measured accuracy of the engine charge temperature becomes increasingly evident for that of point of fall.This paper proposes the method to measure rocket projectile charge substitute material for measuring rocket projectile charge temperature,which overcomes the difficulty resulting from measuring rocket projectile charge temperature and improving the accuracy of measurement,presents how to measure charge temperatur... |
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| Keywords: | substitute material charge temperature measurement analogue |
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