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                    Design and Application of Space-Based MEMS                      331


                       An approach in the same vein emphasizing process monitoring and quality
                    assurance methods has been applied to MEMS components. These methods include
                    techniques to study:

                       (1) Process bias
                       (2) Material microstructure and mechanical properties
                       (3) Mechanical response of spring-supported structures, and
                       (4) Actuator performance


                       Characterization of the as-produced components and materials serves as the
                    starting point for future studies of reliability of MEMS components and systems.
                    Extensive process monitoring is performed at every step. 13
                       In recent years, the POF approach has been used for new and emerging
                    technologies such as multichip modules for insertion into space flight applica-
                    tions. 14  The POF approach has been applied to MEMS reliability by representatives
                    from the French Space Agency, Centre National d’Etudes Spatiales 4,6  and at JPL,
                    Caltech 15  among others.


                    15.4 MEMS FAILURE MECHANISMS
                    MEMS reliability and failure mechanisms concerns for the space environment
                    include: material mismatches, fracture and fatigue, adhesion and stiction, friction
                    and wear, electrostatic interference, radiation damage, and thermal effects.

                    15.4.1 MATERIAL INCOMPATIBILITIES

                    Process incompatibilities, materials issues, and fabrication limitations still present
                    formidable challenges to any practical commercialization of most developmental
                               16
                    microsystems. Processing may induce thermomechanical stresses due to mismatch
                    of the coefficients of thermal expansion (CTE) of the base material. Due to the unique
                    structure and small scale of MEMS, residual stresses during the deposition processes
                    can have a profound effect on the functionality of the structures. Typically, material
                    properties of thin films used in surface micromachining are not controlled during
                    deposition. The residual stress, for example, tends to vary significantly for different
                    deposition methods. Currently, few techniques are available to measure the residual
                    stress in MEMS devices. Differences in stress between the multiple metal and
                    dielectric layers may cause vertical stress gradients and curl. Additionally, misalign-
                    ment between layers may cause lateral stress gradients and curl. This curl that may
                    also be induced through stresses in plating and postprocessing yields, an effect often
                    termed ‘‘potato chipping.’’
                       At all steps, the concerns of material compatibilities will need to be addressed.
                    During packaging of MEMS, stresses will be distributed within the die attach, with
                    die and substrate contributing to the reliability or lack of reliability of the packaging
                    structure. Numerous studies in the literature are available relative to the potential of
                    decreasing or inducing stress during processing steps. 17–20




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