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首页> 外文期刊>Journal of Spacecraft and Rockets >Near-Ultraviolet Emission Spectroscopy During an Airborne Observation of the Stardust Reentry
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Near-Ultraviolet Emission Spectroscopy During an Airborne Observation of the Stardust Reentry

机译:机载星尘折返的空中观测过程中的近紫外光谱。

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摘要

Thermal radiation of the heatshield and the emission of the postshock layer around the Stardust capsule, during its reentry, were detected by a NASA-led observation campaign aboard NASA's DC-8 airborne observatory involving teams from several nations. The German SLIT experiment used a conventional spectrometer, in a Czerny-Turner configuration (300 mm focal length and a 600 lines/mm grating), fed by fiber optics, to cover a wavelength range from 324 to 456 nm with a pixel resolution of 0.08 nm. The reentering spacecraft was tracked manually using a camera with a view angle of 20 deg, and light from the capsule was collected using a small mirror telescope with a view angle of only 0.45 deg. Data were gathered with a measurement frequency of 5 Hz in a 30-s time interval around the point of maximum heating until the capsule left the field of view. The emission of carbon nitride (as a major ablation product), N_2~+ and different atoms were monitored successfully during that time. Because of the nature of the experimental setup, spatial resolution of the radiation field was not possible. Therefore, all measured values represent an integration of radiation from the visible part of the glowing heatshield, and from the plasma in the postshock region. Further, due to challenges in tracking, not every spectrum gathered contained data. The measured spectra can be split up into two parts: 1) continuum spectra, which represent a superposition of the heatshield radiation and the continuum radiation of particles due to microspallation in the plasma, and 2) line spectra from the plasma in the shock layer. Planck temperatures (interpreted as the surface temperatures of the Stardust heatshield) were determined assuming either a constant surface temperature, or a temperature distribution deduced from numerical simulation. The constant surface temperatures are in good agreement with numerical simulations, but the peak values at the stagnation point are significantly lower than those in the numerical simulation if a temperature distribution over the surface is assumed. Emission bands of carbon nitride and N_2~+ were tracked along the visible trajectory and compared with a spectral simulation with satisfying agreement Values for the integrated radiation of the transitions of interest for these species were extracted from this comparison.
机译:在NASA的DC-8空中天文台上,由美国国家航空航天局(NASA)领导的一项观测运动,由来自多个国家的小组,对重入星尘舱后的隔热板的热辐射和震荡层周围的余震层的排放进行了检测。德国SLIT实验使用Czerny-Turner配置(焦距为300 mm,光栅线为600行/ mm)配置的常规光谱仪,由光纤提供,以覆盖324至456 nm的波长范围,像素分辨率为0.08纳米使用摄像机以20度的视角手动跟踪进入的航天器,并使用视角仅为0.45度的小型镜式望远镜收集来自胶囊的光。在最大加热点附近直至30秒的时间间隔内,以30 Hz的时间间隔以5 Hz的测量频率收集数据。在此期间,成功监测了氮化碳(作为主要的烧蚀产物),N_2〜+和不同原子的排放。由于实验装置的性质,不可能实现辐射场的空间分辨率。因此,所有测量值代表了来自发光隔热板可见部分以及来自余震区域中等离子体的辐射的积分。此外,由于跟踪方面的挑战,并非每个收集的频谱都包含数据。测得的光谱可以分为两部分:1)连续光谱,表示由于等离子体中的微散布而引起的隔热屏辐射和颗粒连续辐射的叠加,以及2)来自冲击层中等离子体的线光谱。普朗克温度(被解释为“星尘”隔热板的表面温度)是在假定表面温度恒定或从数值模拟推导出温度分布的情况下确定的。恒定的表面温度与数值模拟非常吻合,但是如果假定表面上的温度分布,则停滞点的峰值显着低于数值模拟中的峰值。沿着可见光轨迹跟踪了氮化碳和N_2〜+的发射带,并与具有令人满意协议的光谱模拟进行了比较,从该比较中提取了这些物种感兴趣的跃迁的积分辐射值。

著录项

  • 来源
    《Journal of Spacecraft and Rockets 》 |2011年第1期| p.59-71| 共13页
  • 作者单位

    NASA Ames Research Center, Moffett Field, California 94035l;

    NASA Ames Research Center, Moffett Field, California 94035l;

  • 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
  • 关键词

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