CR21 line item for the raw composite material used in the body panels.
Now tracked through the laminate weight calculator and the schedule for each panel.
No part-specific design process is documented. The Body Work and Nose subsystem design process applies: 1. Take the outer surface from the aerodynamics CFD geometry so the panel is the same surface that was simulated. 2. Choose a laminate schedule using the team's laminate weight calculator, trading ply count against stiffness and surface finish. 3. Mold: tooling board milled on the 5-axis gantry for large surfaces, 3D printed molds for small parts. Automotive clearcoat over the print cut roughly 22 hours of sanding and made the molds reusable. 4. Layup and cure, then post-process, fill the leading edges with polyester filler and satin clearcoat for UV protection. 5. Test fit on the frame, then trim and drill mounting hardware to jigs.
None recorded. This part has no entry in Knowledge_Transfer/Issue Logging/Fault Vault.xlsx, in either Issue Log.xlsx, in CR22/Issue Tracking/Shakedown 7-15-23.xlsx, or in any design review issue list found in CrimsonStorage or Box.
Nothing in CrimsonStorage covers these yet.