Heat pipes in sandwich structures for spacecrafts
Thermal performance of two different heat pipes is investigated in this study to evaluate the efficiency and feasibility of embedding within simulated satellite substrates subjected to localized heat source. Both experiments and numerical methods were performed to determine the heat transfer capabil...
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2011
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sg-ntu-dr.10356-449552023-03-04T19:21:48Z Heat pipes in sandwich structures for spacecrafts Ng, Benson Guo Loong. Sunil Chandrakant Joshi School of Mechanical and Aerospace Engineering DRNTU::Engineering::Mathematics and analysis::Simulations Thermal performance of two different heat pipes is investigated in this study to evaluate the efficiency and feasibility of embedding within simulated satellite substrates subjected to localized heat source. Both experiments and numerical methods were performed to determine the heat transfer capability. Various experimental setups were performed to determine the effect gravity exert on the performance of the heat pipe by inclining the setups at different angles. With the help of CFX software, numerical analysis were performed under similar real time conditions to determine the heat pipe performance in micro gravity environment, the effect of gravity with different inclination of the setup, the optimum number of embedded heat pipes within the substrate and the effect of distributing the heat pipe into different proportion in the heater plate and substrate plate. Bachelor of Engineering (Aerospace Engineering) 2011-06-07T06:52:00Z 2011-06-07T06:52:00Z 2011 2011 Final Year Project (FYP) http://hdl.handle.net/10356/44955 en Nanyang Technological University 74 p. application/pdf |
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DRNTU::Engineering::Mathematics and analysis::Simulations Ng, Benson Guo Loong. Heat pipes in sandwich structures for spacecrafts |
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Thermal performance of two different heat pipes is investigated in this study to evaluate the efficiency and feasibility of embedding within simulated satellite substrates subjected to localized heat source. Both experiments and numerical methods were performed to determine the heat transfer capability. Various experimental setups were performed to determine the effect gravity exert on the performance of the heat pipe by inclining the setups at different angles. With the help of CFX software, numerical analysis were performed under similar real time conditions to determine the heat pipe performance in micro gravity environment, the effect of gravity with different inclination of the setup, the optimum number of embedded heat pipes within the substrate and the effect of distributing the heat pipe into different proportion in the heater plate and substrate plate. |
author2 |
Sunil Chandrakant Joshi |
author_facet |
Sunil Chandrakant Joshi Ng, Benson Guo Loong. |
format |
Final Year Project |
author |
Ng, Benson Guo Loong. |
author_sort |
Ng, Benson Guo Loong. |
title |
Heat pipes in sandwich structures for spacecrafts |
title_short |
Heat pipes in sandwich structures for spacecrafts |
title_full |
Heat pipes in sandwich structures for spacecrafts |
title_fullStr |
Heat pipes in sandwich structures for spacecrafts |
title_full_unstemmed |
Heat pipes in sandwich structures for spacecrafts |
title_sort |
heat pipes in sandwich structures for spacecrafts |
publishDate |
2011 |
url |
http://hdl.handle.net/10356/44955 |
_version_ |
1759857720117166080 |