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                    Space Radiation Effects and Microelectromechanical Systems       91


                    geomagnetic fields extend to higher latitudes, the exposure to solar particles in the
                    polar regions will be reduced. This will be somewhat compensated by the enhanced
                    cosmic ray flux. Nevertheless, the total radiation exposure will not be as severe as
                    during a period of high solar activity.

                    5.1.3 INTERPLANETARY SPACE
                    Missions in interplanetary space consist of a number of phases, each with a different
                    radiation environment. The first phase typically involves placing the spacecraft into
                    geosynchronous orbit, which requires it to pass through the heart of the Earth’s
                    radiation belts, sometimes more than once. During this first phase, the spacecraft
                    will accumulate a significant radiation exposure. The spacecraft then spends some
                    time in GEO before being injected into its interplanetary orbit. Depending on how
                    long it spends in GEO, the spacecraft and the components on board could experi-
                    ence a substantial total dose due to the electrons in the outer region of the second
                    electron radiation belt. Once the spacecraft has left GEO and is traveling in
                    interplanetary space, it is exposed to radiation from the Sun and from cosmic
                    rays. The total radiation flux is then due to solar activity, the distance between
                    the Sun and the spacecraft, and cosmic ray contributions. The major danger to
                    spacecraft lies in solar particle events that, as noted previously, can lead to an
                    increase in the radiation flux to which a spacecraft is normally exposed by many
                    orders of magnitude.

                    5.1.4 PLANETARY MISSIONS
                    The radiation environment around other planets varies greatly, depending on the
                    strength of their magnetic fields and their distance from the Sun. For instance, the
                    Earth’s moon has no magnetic field and the radiation exposure there does not differ
                    significantly from that in interplanetary space. In contrast, Jupiter’s magnetic field
                    is much stronger than that of the Earth. In addition, Jupiter’s moons orbit within the
                    intense radiation belts, requiring any mission to one of Jupiter’s moons to use parts
                    with a high degree of immunity to radiation and, if necessary, to shield the parts as
                    well. Mars has a very weak magnetic field, which offers little ‘‘shielding’’ against
                    cosmic rays and solar particles. The absence of a magnetic field around Mars also
                    means that spacecraft in orbit around Mars will not encounter radiation belts, such
                    as those on Earth.

                    5.2 RADIATION EFFECTS

                    Before a device can be used in space it must be qualified to ensure that it will
                    survive the rigors of the space environment. Radiation qualification is one of many
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                    different qualification procedures that must be performed. Others include tempera-
                    ture, pressure, and vibration. In the absence of specific guidelines for qualifying
                    MEMS devices for a radiation environment, radiation test engineers make
                    use of standard radiation qualification procedures that have been developed for
                    microelectronics.




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