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Thermal engineering of Mars entry: carbon/carbon non-ablative aeroshell, part 3
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Thermal engineering of Mars entry: carbon/carbon non-ablative aeroshell, part 3
Hickey, G. S.
;
Lih, S.-S.
;
Shih, W.
URI:
http://hdl.handle.net/2014/12681
Date:
2001-07-09
Citation:
International Conference on Environmental Systems
Orlando, FL, USA
Abstract:
This is part three of a development program to evaluate candidate nonablative aeroshell designs.
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JPL TRS 1992+
JPL TRS 1992+
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