Page 95 - MEMS and Microstructures in Aerospace Applications
P. 95

Osiander / MEMS and microstructures in Aerospace applications DK3181_c005 Final Proof page 83  25.8.2005 3:39pm








                         5      Space Radiation

                                Effects and


                                Microelectromechanical


                                Systems




                                Stephen P. Buchner



                    CONTENTS

                    5.1  Introduction.................................................................................................... 83
                        5.1.1 The Space Radiation Environment.................................................... 84
                        5.1.2 Earth Orbits ........................................................................................ 86
                        5.1.3 Interplanetary Space........................................................................... 91
                        5.1.4 Planetary Missions ............................................................................. 91
                    5.2  Radiation Effects ........................................................................................... 91
                        5.2.1 Space Radiation Interaction with Materials and
                              Devices (Ionization)........................................................................... 93
                        5.2.2 Space Radiation Interaction with Materials and Devices
                              (Displacement Damage)..................................................................... 96
                        5.2.3 Radiation Testing of MEMS.............................................................. 97
                    5.3  Examples of Radiation Effects in MEMS .................................................... 97
                        5.3.1 Accelerometer .................................................................................... 98
                        5.3.2 Microengine with Comb Drive and Gears ...................................... 101
                        5.3.3 RF Relay........................................................................................... 103
                        5.3.4 Digital Mirror Device ...................................................................... 105
                    5.4  Mitigation of Radiation Effects in MEMS ................................................. 107
                    5.5  Conclusion ................................................................................................... 107
                    References ........................................................................................................... 108


                    5.1 INTRODUCTION
                    The space environment presents a variety of hazards for spacecraft. Not only are
                    there extremes of temperature and pressure to contend with, but the spacecraft must
                    also withstand a constant onslaught of energetic ionized particles and photons that
                    can damage both the spacecraft and its payload. Atomic oxygen (AO) poses a
                    serious hazard because it corrodes materials with which it comes into contact,
                    causing surface erosion and contamination of the spacecraft. High-energy photons

                                                                                     83

                    © 2006 by Taylor & Francis Group, LLC
   90   91   92   93   94   95   96   97   98   99   100