This page contains miscellaneous information regarding honeycomb structures. Rocket Team has upscope plans to use composite honeycomb sandwich panels for fins. This will reduce the weight of the fins while allowing them to remain stiff and strong.
A document with a great overview of honeycomb sandwich panels in an aerospace application is here.
- one of the main takeaways of this document is that debonding of the core and face laminate can cause failure of a honeycomb sandwich panel.
- This debonding can occur when there is too much pressure (relative to ambient pressure) inside the cells of the honeycomb.
- essentially, this excess pressure pushes up on the laminate face, causing it to disbond from the core.
- By symmetry, we can assume that there is no net force on the other honeycomb cells due to excess pressure. Therefore, the main failure mode of overpressurization is disbond between the face and the core.
Personal notes and journal for other honeycomb research and happenings is here.