Composite materials for payload shroud

AI Thread Summary
Designing a 10" diameter, 48" long payload shroud with an ogive nose cone for a large hobby rocket involves conducting an aeroheating analysis to determine maximum temperatures during ascent. The project requires selecting composite materials, necessitating specific data on thermal conductivity and emissivity to determine the appropriate shroud thickness. Access to ASM materials databases can aid in identifying suitable materials, but the choice should also consider the feasibility of manufacturing within time and cost constraints. The complexity of producing large composite parts means that some materials may be more practical than others, depending on available technology and equipment.
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We are looking at designing a 10" diameter, 48" long payload shroud (Ogive nose cone) for a large hobby rocket. We have done an aeroheating analysis based on the trajectory, so we have the max temp. experienced during ascent at several body points. We want to make the shroud out of composites and in order to size the shroud thickness, we need material property data (thermal conductivity, emissivity) for some yet-to-be identified candidate materials. What materials might we look at? I have access to the ASM materials databases, but I'm not really sure exactly what specific materials I should be targeting.

Any thoughts?
 
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One answer is "target the materials where the manufacturing technology for the part is within your time and cost constraints". Making any part that size from composites is unlikely to be trivial, but some options are a lot more non-trivial than others unless you have access to the right specialist equipment.
 

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