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                    Microelectromechanical Systems and Microstructures in Aerospace  357



                    TABLE 16.2
                    MEMS Sample Test Plan
                    Test Item              Qualification              Acceptance

                    Bond strength   Test method 2023 100% NDBP  Test method 2023 100% NDBP
                    Die shear
                    High-temperature  1508C                   1508C
                     storage
                    Low-temperature   558C                     558C
                     storage
                    Burn-in         100 h total on-time       100 h total on-time
                    Thermal cycle or  Maximum or minimum design  Maximum or minimum design +158C;
                                                         5
                     vacuum           +108C; four cycles 1   10  six cycles thermal cycle
                                      Torr
                    Random vibration  Flight (limit) level þ 3 dB flight  Flight (limit) level flight duration/
                                                                  1
                     level duration   duration/axis; three axes  axis ; three axes
                    Sinusoidal vibration  1.25   flight (limit) level flight  Not required
                     level duration   duration/axis; three axes 4 oct/
                     sweep rate       min
                    Temperature cycle   55 to þ808C            55 to þ 608C
                    Mechanical shock  1.4   flight (limit) level  Not required
                     analysis
                    Structural loads test  1.25   flight (limit) loads 1.4    Not required
                     analysis         flight (limit) loads
                    Thermal shock   Permission requirements   Permission requirements
                    Acoustics level  Flight (limit) level þ 3 dB flight  Not required
                     duration         duration
                    EMI/EMC         Mission dependent (refer to ST5-  Mission dependent (refer to ST5-495-
                                      495-007 for details on type and  007 for details on type and levels of
                                      levels of testing required)  testing required)
                    Conducted emissions
                     conducted
                     susceptibility
                     radiated
                     emissions
                    Radiated
                     susceptibility
                    Magnetics       Mission dependent (refer to ST5-  Mission dependent (refer to ST5-495-
                                      495-007 for details on type and  007 for details on type and levels of
                                      levels of testing required)  testing required)


                    reliability of a MEMS device. Because this is so critical, it is important to package the
                    MEMS devices in a controlled, particle-free environment. Every step from die
                    preparation to package seal must be performed in a class 100 cleanroom environment
                    until the device is safely sealed in a hermetic package. Cleanroom techniques
                    normally reserved for wafer fabrication must be extended for use in probing, die
                    prep, and assembly. Thus, the packaging of the MEMS device is as challenging as
                    building the MEMS die itself. Customers who purchase a raw unpackaged die from a

                    © 2006 by Taylor & Francis Group, LLC
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