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One error I have thought of was the thickness of the carbon fiber was not adjusted in the SolidWorks document to reflect the real thickness of the plates. This could cause issues with size of the aeropanels and the locations of the mounting holes. Something to keep in mind for next iteration.
Author: Evan Janakievski Date: 2024/03/18
New mounting method has been designed, that will allow the cabin to be assembled prior to being attached to the X-Frame.
New aeropanels are under design. Will meet X-Frame at 90 degree angle. Front and back first iteration done, need to work on side panels which could then let Divit finish his design.
Mounting location was not changed for the cabin, it will be the same dimensions apart from shape of the panels.