Influence of ablation on vacuum-ultraviolet radiation in a plasma wind tunnel flow
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...
| Main Authors: | , , , , , |
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| 格式: | Journal article |
| 语言: | English |
| 出版: |
American Institute of Aeronautics and Astronautics
2017
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