| タイトル | Ongoing Capabilities and Developments of Re-Entry Plasma Ground Tests at EADS-ASTRIUM |
| 著者（英） | Jullien, Pierre |
| 著者所属（英） | European Aeronautic Defence and Space Co. |
| 発行日 | 2008-09-22 |
| 言語 | eng |
| 内容記述 | During re-entry, spacecrafts are subjected to extreme thermal loads. On mars, they may go through dust storms. These external heat loads are leading the design of re-entry vehicles or are affecting it for spacecraft facing solid propellant jet stream. Sizing the Thermal Protection System require a good knowledge of such solicitations and means to model and reproduce them on earth. Through its work on European projects, ASTRIUM has developed the full range of competences to deal with such issues. For instance, we have designed and tested the heat-shield of the Huygens probe which landed on Titan. In particular, our plasma generators aim to reproduce a wide variety of re-entry conditions. Heat loads are generated by the huge speed of the probes. Such conditions cannot be fully reproduced. Ground tests focus on reproducing local aerothermal loads by using slower but hotter flows. Our inductive plasma torch enables to test little samples at low TRL. Amongst the arc-jets, one was design to test architecture design of ISS crew return system and others fit more severe re-entry such as sample returns or Venus re-entry. The last developments aimed in testing samples in seeded flows. First step was to design and test the seeding device. Special diagnostics characterizing the resulting flow enabled us to fit it to the requirements. |
| NASA分類 | Spacecraft Design, Testing and Performance |
| 権利 | Copyright, Distribution as joint owner in the copyright |
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