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The goal of our study is to optimize the packaging process of an optical sensor module under the space mission requirements. The intention of the project is to develop a generation of optical sensor modules avoiding conventional organic adhesives (standard used technologies). The sensor module, designed by Sodern, consists of three parts: the sensor, the filter frame and the filter. The Solderjet Bumping is planned to be used for assembling KOVAR(29 % Ni, 17 % Co, 54 % Fe) and N-BK10 (Borosilicate-Kronglas, Schott glass) and for assembling KOVAR and KOVAR materials, chosen for this application, and creation of a strong bond between these materials, which should withstand the harsh environmental space conditions.

Soldering and Packaging Study for an Optical Filter Required for High Resolution Earth Observation Space Missions