Page 323 - MEMS and Microstructures in Aerospace Applications
P. 323

Osiander / MEMS and microstructures in Aerospace applications  DK3181_c014 Final Proof page 317 1.9.2005 12:47pm




                    Material Selection for Applications of MEMS                     317


                       Although much work has been done on characterizing the effects of radiation on
                    microelectronics, little has been done for MEMS devices. It is recommended that
                    gamma, proton, and x-ray testing be done on MEMS devices to better understand
                    the effects on devices destined for flight. Excitation and sensing voltages can
                    be effected by dielectric charging and dielectric failures can be accelerated by
                    radiation effects, and therefore electrostatic devices show the largest sensitivities
                    to radiation. 21–24  Minimizing the use of dielectrics, employing radiation shielding,
                    leaky dielectrics, and grounded conductive planes are mitigation strategies. The
                    reader is referred to the chapter on radiation for further details, but major effects are
                    summarized in Table 14.6.

                    14.5.6 PARTICLES
                    Particulates are fine particles that are prevalent in the atmosphere as well as in
                    space. While particulates generally will not affect hermetically packed MEMS
                    devices, those directly exposed to the space environment will need to be protected.
                    On atmospheric missions dust will potentially clog moveable devices. Meteoroids
                    and other orbital debris will be a concern for MEMS devices on the outside of
                    spacecraft which are exposed to the space environment during orbit.


                    14.5.7 VACUUM
                    In vacuum, polymer materials tend to lose volume as their solvents outgas. All
                    materials intended for spacecraft use must first pass the outgassing data as specified
                    in NASA Reference Publication 1124, revised by the Jet Propulsion Laboratory
                    (JPL) using an apparatus developed at Stanford Research Institute (SRI) that
                    measures the mass loss in vacuum and collects the outgassed products. The original


                    TABLE 14.6
                    Radiation Effects 33

                    Radiation Effect            Cause               Physical Impact
                    Single event upset (SEU)  High energy ions, protons  Formation of electron–hole pairs
                    Single event latch-up (SEL)  High energy ions, protons  Localized high current condition
                                                               in semiconductor materials
                    Single event hard error (SHE)  High energy ions, neutrons,  Permanent localized charging of oxide
                                           protons
                    Single event burnout (SEB)  High energy ions, neutrons,  Increased parasitics
                                           protons
                    Single event gate rupture  High energy ions, neutrons,  Breakdown of oxide insulator
                     (SEGR)                protons
                    Lattice damage       High energy ions, neutrons,  Displacement of lattice atoms; minority
                                           protons             carrier lifetime doping level effects
                    Total ionizing dose (TID)  Electrons, protons  Charge trapping, interface state growth
                                                               at oxide–silicon interfaces






                    © 2006 by Taylor & Francis Group, LLC
   318   319   320   321   322   323   324   325   326   327   328