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 |
| Subjects: | |
| Online Access: | http://bulletin.incas.ro/files/ioan_rusu_v2no4_full.pdf |
| _version_ | 1818493708392202240 |
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| author | Ioan RUSU |
| author_facet | Ioan RUSU |
| author_sort | Ioan RUSU |
| collection | DOAJ |
| description | 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 author Ioan Rusuhas discovered by simply researches that the Coanda effect could be /extended also to the fluid flowon discontinuous solids, namely, on solids provided with orifices. This phenomenon was named by theauthor, the expanded Coanda effect. Starting with this discovery, the author has invented a thermalshield, registered at The State Office for inventions and Trademarks OSIM, deposit F 2010 0153This thermal shield:- is built as a covering rocket sheet with many orifices installed with a minimum space fromthe rocket body- takes over the heat fluid generated by the frontal part of the rocket and avoids the directcontact between the heat fluid and the rocket body- ensures the evacuation of the infrared radiation, generated by the heat fluid flowing overthe shield because of the extended Coanda effect by reflection from the rocket bodysurface. |
| first_indexed | 2024-12-10T17:57:31Z |
| format | Article |
| id | doaj.art-5903b5a355b44ba8ae094bbaca894359 |
| institution | Directory Open Access Journal |
| issn | 2066-8201 2247-4528 |
| language | English |
| last_indexed | 2024-12-10T17:57:31Z |
| publishDate | 2010-12-01 |
| publisher | National Institute for Aerospace Research “Elie Carafoli” - INCAS |
| record_format | Article |
| series | INCAS Bulletin |
| spelling | doaj.art-5903b5a355b44ba8ae094bbaca8943592022-12-22T01:38:53ZengNational Institute for Aerospace Research “Elie Carafoli” - INCASINCAS Bulletin2066-82012247-45282010-12-012417317810.13111/2066-8201.2010.2.4.22Antithermal shield for rockets with heat evacuation by infrared radiation reflectionIoan RUSUAt 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 author Ioan Rusuhas discovered by simply researches that the Coanda effect could be /extended also to the fluid flowon discontinuous solids, namely, on solids provided with orifices. This phenomenon was named by theauthor, the expanded Coanda effect. Starting with this discovery, the author has invented a thermalshield, registered at The State Office for inventions and Trademarks OSIM, deposit F 2010 0153This thermal shield:- is built as a covering rocket sheet with many orifices installed with a minimum space fromthe rocket body- takes over the heat fluid generated by the frontal part of the rocket and avoids the directcontact between the heat fluid and the rocket body- ensures the evacuation of the infrared radiation, generated by the heat fluid flowing overthe shield because of the extended Coanda effect by reflection from the rocket bodysurface.http://bulletin.incas.ro/files/ioan_rusu_v2no4_full.pdfantithermalthermal shieldCoanda effect |
| spellingShingle | Ioan RUSU Antithermal shield for rockets with heat evacuation by infrared radiation reflection INCAS Bulletin antithermal thermal shield Coanda effect |
| title | Antithermal shield for rockets with heat evacuation by infrared radiation reflection |
| title_full | Antithermal shield for rockets with heat evacuation by infrared radiation reflection |
| title_fullStr | Antithermal shield for rockets with heat evacuation by infrared radiation reflection |
| title_full_unstemmed | Antithermal shield for rockets with heat evacuation by infrared radiation reflection |
| title_short | Antithermal shield for rockets with heat evacuation by infrared radiation reflection |
| title_sort | antithermal shield for rockets with heat evacuation by infrared radiation reflection |
| topic | antithermal thermal shield Coanda effect |
| url | http://bulletin.incas.ro/files/ioan_rusu_v2no4_full.pdf |
| work_keys_str_mv | AT ioanrusu antithermalshieldforrocketswithheatevacuationbyinfraredradiationreflection |