Journal article
Influence of ablation on vacuum-ultraviolet radiation in a plasma wind tunnel flow
- Abstract:
- Plasma wind tunnel experiments have been performed simulating a Hayabusa reentry trajectory point at 78.8 km altitude with a velocity of 11.7 km/s corresponding to a local mass–specific enthalpy of 68.4 MJ/kg and a stagnation pressure of 2.44 kPa. Ablation–radiation coupling is investigated using a carbon preform sample, a lightweight carbon phenolic ablator sample, and cooled copper. Optical emission spectroscopic measurements in the vacuum ultraviolet (VUV) regime (116–197 nm) have been conducted through a bore hole in the stagnation point of the different samples. Optical emission spectroscopic measurements in the UV/VIS spectral range (320–810 nm) have been conducted viewing the plasma from the side. The stagnation point VUV radiation to the carbon preform sample is strongest, whereas it is weakest for the carbon phenolic sample. In the UV/VIS both carbon-based material samples lead to stronger plasma radiation than copper. Atomic number densities in front of the samples are largest for the carbon preform sample and lowest for the carbon phenolic sample. Rotational and vibrational temperatures are lower for both the carbon-based materials compared with copper. The measurements show for the first time experimentally the radiative heat flux mitigation by carbon phenolic materials.
- Publication status:
- Published
- Peer review status:
- Peer reviewed
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- Files:
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(Preview, Accepted manuscript, 3.1MB, Terms of use)
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- Publisher copy:
- 10.2514/1.t4936
Authors
- Publisher:
- American Institute of Aeronautics and Astronautics
- Journal:
- Journal of Thermophysics and Heat Transfer More from this journal
- Volume:
- 31
- Issue:
- 3
- Pages:
- 575-585
- Publication date:
- 2017-01-20
- Acceptance date:
- 2016-08-26
- DOI:
- EISSN:
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1533-6808
- ISSN:
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0887-8722
- Language:
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English
- Keywords:
- Pubs id:
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1159640
- Local pid:
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pubs:1159640
- Deposit date:
-
2021-02-01
Terms of use
- Copyright holder:
- Hermann et al.
- Copyright date:
- 2017
- Rights statement:
- © 2016 by the authors. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission.
- Notes:
- This is the accepted manuscript version of the article. The final version is available from American Institute of Aeronautics and Astronautics at: https://doi.org/10.2514/1.T4936
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