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A inconel turbo wrap would do too well of a job, and that ceramic coating hold enough heat in the manifold to provide a high and low pressure gradient across the turbine, but also allow enough heat to dissipate through the manifold VIA radiation to disallow heat destroying the CHRA and possibly heads... I figured that leaving the DP exposed, perhaps even applying thermal dispersant, would aid in getting the heat out as quickly as possible and take advantage of faster spooling. What do you feel about that? Would you recommend heat wrapping the manifold if ceramic coating was not available? I'm sitting on some DEI titanium wrap...
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