UAV and drone structures
Wings, fuselage panels, booms and control surfaces where a stiff sandwich skin has to stay light. Grade and thickness depend on the load case and the cure cycle.
Applications
PMI structural foam is considered wherever a composite sandwich needs stiffness at low weight. The scenarios below describe inquiry directions, not published case studies.
No customer names, project names, supplied quantities or performance results are published on this site. Availability and suitability for your application are confirmed per inquiry.
Wings, fuselage panels, booms and control surfaces where a stiff sandwich skin has to stay light. Grade and thickness depend on the load case and the cure cycle.
Radome and antenna structures use foam cores where structural performance and dielectric behaviour both matter. Requirements are confirmed per project.
Buoyancy modules and float bodies, including the buoyancy grades listed by the manufacturer. Density, water exposure and finish are confirmed per inquiry.
Core formats for blade shells and structural components. Supply format, sheet size and grade availability are confirmed per inquiry.
Sandwich components for airframes, wings and near-space platforms. The grade, documentation and process cycle are confirmed per project.
Thin sheet cores for model aircraft and small unmanned structures. Thickness availability and sheet format are confirmed per inquiry.
Selection
Describe the part, the process and the core format you need. We will confirm availability and the next step.