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                    Vision for Microtechnology Space Missions                        33


                    disruptive technological impact of MEMS on how space systems are designed,
                    built, and operated. One option is to adopt a technology infusion approach similar to
                    the one the Defense Advanced Research Projects Agency (DARPA) has pursued for
                    the development and widespread integration of MEMS-based microsystems to
                    revolutionize our military’s capabilities on future battlefields. Technologists, re-
                    searchers, and decision makers interested in developing truly innovative and enab-
                    ling MEMS-based microsystems that will support the VSE goals of affordability,
                    reliability, effectiveness, and flexibility would do well to study the DARPA ap-
                    proach, where multiple high-risk or high-payoff military MEMS technologies are
                    being pursued to dramatically improve the agility, accuracy, lethality, robustness,
                    and reliability of warfighter systems.
                       Transitioning MEMS microsystems and devices out of the laboratory and into
                    operational space systems will present many challenges. Clearly much has been
                    accomplished but several critical issues remain to be resolved in order to produce
                    MEMS microsystems that will satisfy the demanding performance and environ-
                    mental requirements of space missions. In the spirit of Rear Admiral Grace Murray
                    Hopper (who is quoted as saying ‘‘If it’s a good idea, go ahead and do it. It’s much
                    easier to apologize than it is to get permission’’) the community must continue to
                    innovate with open minds for if we constrain our vision for MEMS in space, an
                    opportunity may be missed to bend (or even break) current space platform design
                    and production paradigms.


                    REFERENCES
                     1. Osiander, R., S.L. Firebaugh, J.L. Champion, et al., Microelectromechanical devices for
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                     2. Wesolek, D.M., J.L. Champion, F.A. Hererro, et al., A micro-machined flat plasma
                       spectrometer (FlaPS), Proceedings of SPIE — The International Society for Optical
                       Engineering 5344, pp. 89 (2004).
                     3. Sillon, N. and R. Baptist, Sensors and actuators B (chemical), Proceedings of 11th
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                     4. Mott, D.B., R. Barclay, A. Bier, et al., Micromachined tunable Fabry–Perot filters for
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                       Engineering 4841, pp. 578 (2002).
                     5. George, T., Overview of MEMS/NEMS technology development for space applications
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                       determination, 16th Annual AIAA/USU Conference on Small Satellites, Logan, UT (2002).
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                       Mechanics (SEM) Annual Conference (2003).
                     8. Connelly, J.A., et al., Alignment and performance of the infrared multi-object spectrom-
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