Composite materials for payload shroud

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SUMMARY

The discussion focuses on designing a 10" diameter, 48" long payload shroud (Ogive nose cone) for a large hobby rocket using composite materials. Key considerations include conducting an aeroheating analysis to determine maximum temperatures during ascent and identifying candidate materials based on their thermal conductivity and emissivity. The participant has access to ASM materials databases but seeks guidance on specific materials that align with manufacturing technology constraints. The consensus emphasizes the importance of selecting materials that are feasible within time and cost limits while considering the complexity of composite manufacturing.

PREREQUISITES
  • Understanding of composite materials and their properties
  • Familiarity with aeroheating analysis techniques
  • Knowledge of thermal conductivity and emissivity concepts
  • Experience with the ASM materials databases
NEXT STEPS
  • Research composite materials suitable for high-temperature applications
  • Explore manufacturing techniques for large composite structures
  • Investigate thermal property databases for candidate materials
  • Learn about the design considerations for payload shrouds in rocketry
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Engineers, materials scientists, and hobby rocket enthusiasts involved in the design and manufacturing of composite structures for aerospace applications.

engineer23
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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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