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[1]段文浩,于 涛,杨 莹.辐射式热流测量系统及其应用[J].火箭推进,2014,40(01):85-91.
　DUAN Wen-hao,YU Tao,YANG Ying.Radiant heat flux measuring system and its application[J].Journal of Rocket Propulsion,2014,40(01):85-91.
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辐射式热流测量系统及其应用

《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V] 卷: 40 期数: 2014年01期 页码: 85-91 栏目: 测控与试验 出版日期: 2014-02-28
Title:
Radiant heat flux measuring system and its application
作者:
段文浩1; 于 涛1; 杨 莹2
1. 北京航天试验技术研究所，北京 100074；2. 北京航天动力研究所，北京 100076
Author(s):
DUAN Wen-hao1;  YU Tao1;  YANG Ying2
1. Beijing Institute of Aerospace Testing Technology, Beijing 100074, China; 2. Beijing Aerospace Propulsion Institute, Beijing, 100076, China
关键词:
火箭发动机; 模拟热真空试验; 热流测量; 辐射
Keywords:
rocket engine;  simulation thermal vacuum test;  heat flux measurement;  radiation
分类号:
V433.9-34
文献标志码:
A
摘要:
根据某型号发动机进行的地面模拟热真空环境试验要求，建立了热真空环境模拟系统，在分析热流测量原理的基础上，应用一套辐射式热流测量系统对试验时发动机周围的热流进行测量。着重介绍系统组成及工作原理，热流测量传感器的标定方法。通过热辐射装置热流分布的计算和实际测量结果对比，验证了热流测量系统获取数据真实。
Abstract:
According to the requirements of ground simulation thermal vacuum test for a certain type of rocket engine, the thermal vacuum environment simulation system was established. On the basis of analyzing the heat measurement principle, a radiant heat flux measurement system was used to test the heat flux around the engine while the engine was working. The system composition, working principle, the calibration method of heat flux measurement sensor are introduced emphatically in this article. Through the comparison between the heat flux distribution calculation of thermal radiation device and the results of actual measurement, the facticity and reliability of the data got by the heat flux measuring system was verified.

参考文献/References:

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备注/Memo

收稿日期：2013-08-07；修回日期：2013-09-26 作者简介：段文浩（1986—），男，助理工程师，研究领域为火箭发动机试验测控技术

更新日期/Last Update: 1900-01-01