Publication Date:
2019-07-13
Description:
Performance prediction of fixed wing leading edges radiative, ablative and active cooling thermal protection systems and system weights comparison for space shuttle entry mission
Keywords:
SPACE VEHICLES
Type:
AIAA PAPER 71-445
,
THERMOPHYSICS CONFERENCE; Apr 26, 1971 - Apr 28, 1971; TULLAHOMA, TN
Format:
text
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