Space. Deep space optical communication (laser) aperture cover assembly.
Previous structures were heavy aluminum constructions. By converting to a composite/metallic hybrid structure, the customer was able to save significant mass while retaining their preferred method of aperture cover deployment.
This optics enclosure is part of a probe that is operating at extremely high and low temperatures. By selecting a hybrid structure, the customer acquired certain operational benefits but took on extra complexity due to the inherent CTE variations between metallic and composite materials. This was further complicated by an extremely tight schedule.
Near zero CTE precision optics for space applications have been prohibitively expensive for commercial ventures. Stiffness and CTE requirements mandated use of expensive materials and processes.