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Thermal engineering of Mars entry: carbon/carbon non-ablative aeroshell, part 3

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dc.contributor.author Hickey, G. S. en_US
dc.contributor.author Lih, S.-S. en_US
dc.contributor.author Shih, W. en_US
dc.date.accessioned 2004-09-22T22:51:22Z
dc.date.available 2004-09-22T22:51:22Z
dc.date.issued 2001-07-09 en_US
dc.identifier.citation International Conference on Environmental Systems en_US
dc.identifier.citation Orlando, FL, USA en_US
dc.identifier.clearanceno 01-0981 en_US
dc.identifier.uri http://hdl.handle.net/2014/12681
dc.description.abstract This is part three of a development program to evaluate candidate nonablative aeroshell designs. en_US
dc.format.extent 587968 bytes
dc.format.mimetype application/pdf
dc.language.iso en_US
dc.subject.other carbon-carbon aeroshell aerogel en_US
dc.title Thermal engineering of Mars entry: carbon/carbon non-ablative aeroshell, part 3 en_US


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