MATEC Web of Conferences
Volume 61, 2016The International Seminar on Applied Physics, Optoelectronics and Photonics (APOP 2016)
|Number of page(s)||5|
|Section||Chapter 4 Information Technology|
|Published online||28 June 2016|
Heat-balance Thermal Protection with Heat Pipes for Hypersonic Vehicle
1 Engineering University of the Armed Police Force, Xi’an 710086, PR China
2 National University of Defense Technology, Changsha 410073, PR China
a Corresponding author: firstname.lastname@example.org
Heat-balance thermal protection is non-ablating thermal protection for leading edge of hypersonic vehicle. Heat will be quickly transferred from high aerodynamic heating area to low aerodynamic heating area, where the energy will be released by radiation. The temperature of high aerodynamic heating area could be reduced to protect the designed structure from being burned down. Heat-balance thermal protection is summarized. The research on heat-pipe for heat-balance thermal protection is introduced.
Key words: Heating Heat-balance Thermal Protection / Heat-pipe / Hypersonic / Aerodynamic Heating
© Owned by the authors, published by EDP Sciences, 2016
This is an Open Access article distributed under the terms of the Creative Commons Attribution License 4.0, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.
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