Assessment of Carbon-Phenolic-in-Air Chemistry Models for Atmospheric Reentry
- Martin, Alexandre
- Boyd, Iain D.
DOIAbstract
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/83605/1/AIAA-2010-4656-637.pd
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/83605/1/AIAA-2010-4656-637.pd
During the atmospheric entry of a blunt body, a bow shock wave is generated on the nose of the vehic...
Protecting a spacecraft during atmospheric entry is one of highest risk factors that needs to be mit...
Two sets of finite-rate gas-surface interaction model between air and the carbon surface are studied...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/83619/1/AIAA-2010-1175-298.pd
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/90646/1/AIAA-2011-143-915.pd
Re-entry vehicles designed for space exploration are usually equipped with thermal protection system...
Recent and future re-entry vehicle designs use ablative material as the main component of the heat s...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/97141/1/AIAA2012-814.pd
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/90680/1/AIAA-2011-3125-594.pd
Peer Reviewedhttps://deepblue.lib.umich.edu/bitstream/2027.42/140697/1/1.T4184.pd
Charring ablators remain the premium choice for space exploration missions that involve atmospheric ...
The great majority of modern space vehicles designed for planetary exploration use ablative material...
Peer Reviewedhttps://deepblue.lib.umich.edu/bitstream/2027.42/140698/1/1.T4202.pd
Vehicles entering planetary atmospheres at high speed require an ablative heat shield in order to wi...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76855/1/AIAA-2008-3805-224.pd
During the atmospheric entry of a blunt body, a bow shock wave is generated on the nose of the vehic...
Protecting a spacecraft during atmospheric entry is one of highest risk factors that needs to be mit...
Two sets of finite-rate gas-surface interaction model between air and the carbon surface are studied...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/83619/1/AIAA-2010-1175-298.pd
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/90646/1/AIAA-2011-143-915.pd
Re-entry vehicles designed for space exploration are usually equipped with thermal protection system...
Recent and future re-entry vehicle designs use ablative material as the main component of the heat s...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/97141/1/AIAA2012-814.pd
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/90680/1/AIAA-2011-3125-594.pd
Peer Reviewedhttps://deepblue.lib.umich.edu/bitstream/2027.42/140697/1/1.T4184.pd
Charring ablators remain the premium choice for space exploration missions that involve atmospheric ...
The great majority of modern space vehicles designed for planetary exploration use ablative material...
Peer Reviewedhttps://deepblue.lib.umich.edu/bitstream/2027.42/140698/1/1.T4202.pd
Vehicles entering planetary atmospheres at high speed require an ablative heat shield in order to wi...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76855/1/AIAA-2008-3805-224.pd
During the atmospheric entry of a blunt body, a bow shock wave is generated on the nose of the vehic...
Protecting a spacecraft during atmospheric entry is one of highest risk factors that needs to be mit...
Two sets of finite-rate gas-surface interaction model between air and the carbon surface are studied...
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