NASA Technical Reports Server (NTRS) 19990018937: 1-D Transient Thermal Modeling of an Ablative Material (MCC-1) Exposed to a Simulated Convective Titan 4 Launch Environment

16 Pages·0.37 MB·English

by  NASA Technical Reports Server (NTRS)

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Conditions ( q"cw = 4.6 Btu/s/ft 2,AI thickness = 0.125 in., MCC-1 thickness =0.158 in.)
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