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                   134                       MEMS and Microstructures in Aerospace Applications


                   product of the current in the magnetometer, which can be chosen depending on the
                   field to be detected, limited only by the current-carrying capability of the material,
                   and the absence of any offset other than the detection limit of the Brownian motion
                   of the resonator itself. It also can be used to detect AC magnetic fields with the same
                                               28
                   narrow bandwidth and sensitivity.
                       The measurement of electric fields in space is important to investigate wave
                   processes in space plasma. To our knowledge, the only micromachined device
                   reported for measurements of electric fields for microsatellites is based on a split
                   Langmuir probe, consisting of two conductive plates in a small distance. 12  Such a
                   prototype was tested on board of the Prognoz-10 satellite.


                   7.3 TELESCOPES AND SPECTROMETERS

                   The development of optical MEMS components during the telecom boom of the
                   late 1990s, has provided building blocks for a new generation of space-based
                   optical devices. Micromachined silicon slits and apertures provide a high degree
                   of precision for critical optical paths, and have been used in space flight dual slit
                   spectrometers. A MEMS Fabry–Perot (FP) interferometer has been developed at
                   NASA GSFC,  29  and additional spectrometers with surface micromachined grating
                   structures controlled via small MEMS motors have been reported. 30  More dramat-
                   ically, microoptoelectromechanical systems (MOEMS) can deflect certain image
                   areas to a spectrometer, can block other areas, or can be used to correct for optical
                   aberrations in the telescope or the instrument. An example is the Near Infrared
                   Spectrograph (NIRSpec) for the JWST, planned for launch in 2009, which will have
                                                               31–34
                   MOEMS devices as an integral part of the instrument.
                       Another application, and one that is relatively well established, is in bolometers.
                   Here, the small pixel size enabled by MEMS and the resulting small thermal
                   capacities allow for integration of large arrays of very small bolometric devices
                   which can be used to detect radiation from the millimeter wave range all the way up
                   to x-rays and particles. 35



                   7.3.1 THE JAMES WEBB SPACE TELESCOPE NEAR-IR SPECTROGRAPH
                   The study of galaxy formation, clustering, chemical abundances, star formation
                   kinematics, active galactic nuclei, young stellar clusters, and measurements of the
                   initial mass function of stars (IMF) requires a near-infrared spectrograph. The
                   NIRSpec for the JWST (in earlier publications referred to as Next Generation
                   Space Telescope or NGST) will be the spectrograph in the wavelength range of
                   0.6 to 5 mm, providing three observation modes with a FOV of ~3.4   3.4
                   arcmin in the current design. In the R~1000 modes, NIRSpec provides users of
                   JWST with the ability to obtain simultaneous spectra of more than 100 objects in a
                   >9 square arcminute FOV. Three gratings cover the wavelength range from 1 to
                   5 mm, and the spectrograph will take advantage of a MEMS shutter system to
                   enable users to observe hundreds of different objects in a single FOV. The European




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