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Visible and Near Infrared Spectroscopy of Hayabusa Reentry Using Semi-Autonomous Tracking

机译:ab鸟折返的可见和近红外光谱半自动跟踪

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摘要

A ground-based tracking camera and coaligned slitless spectrograph were used to measure the spectral signature of visible radiation emitted from the Hayabusa capsule as it entered into the Earth's atmosphere in June 2010. Good quality spectra were obtained, which showed the presence of radiation from the heat shield of the vehicle and the shock-heated air in front of the vehicle. An analysis of the blackbody nature of the radiation concluded that the peak average temperature of the surface was about (3100 ± 100) K. Line spectra from oxygen and nitrogen atoms were used to infer a peak average shock-heated gas temperature of around (7000 ± 400) K.
机译:2010年6月,Hayabusa胶囊进入地球大气层时,使用了基于地面的跟踪摄像头和共对准的无狭缝光谱仪来测量从Hayabusa胶囊发射出的可见辐射的光谱特征。车辆的隔热板和车辆前方的冲击热空气。对辐射黑体性质的分析得出的结论是,表面的峰值平均温度约为(3100±100)K。氧和氮原子的线谱用于推断峰值平均激波加热的气体温度约为(7000) ±400)K。

著录项

  • 来源
    《Journal of Spacecraft and Rockets》 |2014年第1期|31-38|共8页
  • 作者单位

    University of Queensland, Brisbane, Queensland 4072, Australia;

    University of Queensland, Brisbane, Queensland 4072, Australia;

    University of Queensland, Brisbane, Queensland 4072, Australia;

    University of Queensland, Brisbane, Queensland 4072, Australia;

    University of Southern Queensland, Toowoomba, Queensland 4350, Australia;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
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