Page 150 - MEMS and Microstructures in Aerospace Applications
P. 150

Osiander / MEMS and microstructures in Aerospace applications  DK3181_c007 Final Proof page 139 1.9.2005 12:04pm




                    Microtechnologies for Science Instrumentation Applications      139


                       A similar program proposed by JPL is the Advanced Segmented Silicon Space
                    Telescope (ASSiST), which utilizes thin silicon wafers as the building blocks of
                    highly segmented space telescope primary mirrors. 59–61  Using embedded MEMS
                    actuators operating with high bandwidth control, this technology can achieve
                    diffraction-limited image quality in the 3–300 mm wavelength range. The use of
                    silicon wafers as cryogenic mirror segments is carried forward considering a point
                    design of a future NASA ORIGINS mission. Individual segments of the ASSiST
                    consist of 1-mm thick, 300-mm diameter silicon wafers with 10-mm deep
                    frames, assembled into 3-m diameter rafts. This achieves considerable reductions
                    in primary mirror mass through the elimination of a heavy back plane support
                    structure. Rather, they exploit the micromachining capabilities of silicon
                    processing technology to achieve sophisticated control of a highly segmented
                    mirror using high-bandwidth, high-stroke MEMS actuators, which will ultimately
                    be built directly into the mirror segment, resulting in an integrated optics package.
                    Thus, a single segment can perform the traditional light-focusing function of a
                    telescope as well as the control functions, and quite possibly the space deployment
                    functions.


                    7.3.3 SPECTROMETER APPLICATIONS
                    The size of spectrometers, especially infrared spectrometers, has been rapidly
                    reduced in recent years due to uncooled IR detectors with ultrasmall pixel size
                    and modern micromachining techniques. 62  Infrared spectrometers are some of the
                    most important instruments since most molecules show a characteristic ‘‘finger-
                    print’’ spectrum within this range. A reduction in size for these instruments will
                    have a major impact on space-based observations, as well as for terrestrial sensors
                    for chemical and biological agent detection. One example is a Fabry–Perot (FP)-
                                     63
                    based interferometer.  A FP interferometer or etalon consists of two flat, parallel,
                    semitransparent plates coated with films of high reflectivity and low absorption.
                    The pass band of the etalon is determined by the separation between the plates,
                    which is generally varied using piezoelectric actuators. For any large aperture wide
                    field telescope, low-resolution FPs are an ideal option for narrow-band imaging as
                    opposed to linear or circular variable interference filters as they ease size require-
                    ments on filter wheels and offer flexibility in choice of spectral resolution. Tunable
                    filters on space telescopes will require operation at cryogenic temperatures, where
                    piezo actuators alone do not provide sufficient translation to tune the etalon over the
                    desired orders of interference without becoming large and cumbersome. In addition,
                    low-resolution infrared etalons require cavity spacings on the order of a micron.
                    Figure 7.10 and Figure 7.11 show a photograph and the schematic of a FP interfer-
                    ometer design developed at NASA GSFC. 29
                       In this design, the mechanism is fabricated in two sections that are assembled
                    into the final FP filter. The stationary mirror structure consists of a micromachined
                    350-mm thick silicon wafer coated with a multilayer dielectric (MLD) in the
                    aperture. The moving mirror structure is also machined from a 350-mm thick silicon
                    wafer and is identically coated with MLD over its aperture. Its reflector is attached




                   © 2006 by Taylor & Francis Group, LLC
   145   146   147   148   149   150   151   152   153   154   155