Temperature Measurement of HEK-X Expansion Tube Flow by Laser Absorption Spectroscopy

IF 0.7 4区 工程技术 Q4 ENGINEERING, AEROSPACE Transactions of the Japan Society for Aeronautical and Space Sciences Pub Date : 2021-01-01 DOI:10.2322/TJSASS.64.193
M. Matsui, R. Kobayashi, Takashi Okamoto, Kazuhiko Yamada, H. Tanno
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引用次数: 2

Abstract

An expansion tube is a promising facility to simulate atmospheric entry conditions, although its fl ow conditions have not been completely characterized mainly owing to its short operation time. In this study, laser absorption spectroscopy was applied to diagnose HEK-X expansion tube fl ow in the Kakuda Space Center. The target is an absorption line of an oxygen molecule at 763nm. To increase the sensitivity, optical path length was extended by fi ve times using mirrors. Con-sequently, an absorption pro fi le with a fractional absorption of 2.4 « 0.3% was detected at a shock velocity of 7.65 « 0.05km / s. The estimated translational temperature from the Voigt fi tting was 2750 « 450K.
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激光吸收光谱法测量HEK-X膨胀管流动温度
膨胀管是一种很有前途的模拟大气入口条件的设备,但由于其运行时间短,其流动条件尚未完全表征。本研究采用激光吸收光谱法对Kakuda航天中心的HEK-X膨胀管流动进行了诊断。目标是一个氧分子在763nm处的吸收线。为了提高灵敏度,利用反射镜将光路长度延长了5倍。因此,在7.65 ~ 0.05km / s的冲击速度下,检测到分数吸收曲线为2.4 ~ 0.3%。Voigt拟合估计的平移温度为2750 ~ 450K。
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来源期刊
CiteScore
1.80
自引率
0.00%
发文量
18
审稿时长
>12 weeks
期刊介绍: Information not localized
期刊最新文献
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