Characterization of a Reentry Plasma Wind-Tunnel Flow with Vacuum-Ultraviolet to Near-Infrared Spectroscopy

被引:19
|
作者
Hermann, Tobias [1 ]
Loehle, Stefan [1 ]
Zander, Fabian [1 ]
Fulge, Hannes [1 ]
Fasoulas, Stefanos [2 ]
机构
[1] Univ Stuttgart, High Enthalpy Flow Diagnost Grp, Inst Raumfahrtsyst, Pfaffenwaldring 29, D-70569 Stuttgart, Germany
[2] Univ Stuttgart, Inst Raumfahrtsyst, Pfaffenwaldring 29, D-70569 Stuttgart, Germany
关键词
STAGNATION-POINT; CROSS-SECTIONS; ARCJET FLOW; RADIATION; NITROGEN; ENTRY; INTENSITY; ABLATION; AIR;
D O I
10.2514/1.T4695
中图分类号
O414.1 [热力学];
学科分类号
摘要
This paper presents the analysis of optical emission spectroscopic measurements from vacuum ultraviolet (120 nm) to near infrared (960 nm) in a high-enthalpy air plasma flow corresponding to superorbital reentry conditions. The vacuum ultraviolet measurements have been realized with a new experimental setup allowing measurements through a bore hole in the sample. Using the commonly applied optical emission spectroscopy from the side, the radiation transport along the line of sight of the vacuum ultraviolet measurements has been assessed. This allowed the determination of the local ground state densities of atomic oxygen and atomic nitrogen from a branching ratio analysis and the blackbody limiting correction of the vacuum ultraviolet radiation. Through the analysis of the absorption in the borehole, the spectra have been corrected, resulting in a stagnation point radiative heat flux in the vacuum ultraviolet of 235 kW/m(2).
引用
收藏
页码:673 / 688
页数:16
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