Antithermal shield for rockets with heat evacuation by infrared radiation reflection
At high speed, the friction between the air mass and the rocket surface causes a localheating of over 1000 Celsius degrees. For the heat protection of the rocket, on its outside surfacethermal shields are installed.Studying the Coanda effect, the fluid flow on solids surface, respectively, the autho...
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| Format: | Article |
| Language: | English |
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National Institute for Aerospace Research “Elie Carafoli” - INCAS
2010-12-01
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| Series: | INCAS Bulletin |
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| Online Access: | http://bulletin.incas.ro/files/ioan_rusu_v2no4_full.pdf |