Page 342 - MEMS and Microstructures in Aerospace Applications
P. 342

Osiander / MEMS and microstructures in Aerospace applications  DK3181_c015 Final Proof page 335 1.9.2005 12:52pm




                    Design and Application of Space-Based MEMS                      335



                           TABLE 15.1
                           Environmental Factors Checklist (Typical)
                           Natural Occurring             Application Induced

                           Albedo, planetary IR        Acceleration
                           Electromagnetic radiation   Chemicals
                           Electrostatic discharge     Corona
                           Gravity, low                Electromagnetic, laser
                           Humidity, high              Electromagnetic radiation
                           Ionized gases               Electrostatic discharge
                           Magnetics, geo              Explosion
                           Meteoroids                  Icing
                           Particulate levels, high    Magnetics
                           Pollution, air              Moisture
                           Pressure, high              Nuclear radiation
                           Pressure, low, vacuum       Particulate levels, high
                           Radiation, cosmic, soar     Shock, pyro, thermal
                           Temperature, high           Space debris
                           Temperature, low            Temperature, high, aero. heating, fire
                                                       Temperature, low, aero. cooling
                                                       Turbulence
                                                       Vapor trails (plumes)
                                                       Vibration, mechanical, microphonics
                                                       Vibration, acoustic


                    may be able to ignore some other factors. Other natural environmental concerns are
                    seen in a long duration balloon or unmanned aerial vehicles (UAV) type applica-
                    tions but primarily lower atmosphere and terrestrial could include: wind, rain, salt
                    spray, sand and dust, sleet, snow, hail, lightning, ice, fog, clouds, freezing rain,
                    frost, and fungus.

                    15.5.1 COMBINATIONS OF ENVIRONMENTALLY INDUCED STRESSES
                    Concurrent (combined) environments may be more detrimental to reliability than
                    the effects of a single environment. In characterizing the design process, design
                    or test criteria must consider both single and/or combined environments in antici-
                    pation of providing the hardware capability to withstand the hazards identified
                    in the system profile. The synergistic effects of typical combined environments
                    can be illustrated in a matrix relationship, which shows combinations where the
                    total effect is more damaging than the cumulative effect of each environment
                    acting independently. For example, an item may be exposed to a combination
                    such as temperature, humidity, altitude, shock, and vibration while it is being
                    transported. The acceptance to end-of-life history of an item must be examined
                    for these effects. Table 15.2 provides reliability considerations for pairs of envir-
                    onmental factors. 29




                    © 2006 by Taylor & Francis Group, LLC
   337   338   339   340   341   342   343   344   345   346   347