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                    Microelectromechanical Systems and Microstructures in Aerospace Applications  5


                    several types of MEMS microthrusters and characterize their performance, and to
                    fly MEMS microthrusters in space and verify their performance during launch,
                    flight, and landing.

                    1.3.2 PICOSATELLITE MISSION
                    Six picosatellites, part of the payload on OPAL, were launched on January 26, 2000
                    at Vandenberg Air Force Base. The picosatellites were deployed on February 4,
                    2000 and performed for 6 days until February 10, 2000, when the batteries were
                    drained. Rockwell Science Center (RSC) designed and implemented a MEMS-
                    based radio frequency switch experiment, which was integrated into the miniature
                    satellite (picosat) as an initial demonstration of MEMS for space applications. This
                    effort was supported by DARPA Microsystems Technology Office (MTO), and the
                    mission was conducted with Aerospace Corporation and Stanford University as
                    partners. MEMS surface-micromachined metal contacting switches were manufac-
                    tured and used in a simple experiment aboard the miniature satellites to study the
                    device behavior in space, and its feasibility for space applications in general. During
                    the entire orbiting period, information was collected on both the communications
                    and networking protocols and MEMS RF switch experiments. The performance of
                    RF switches has been identical to their performance before the launch. 3

                    1.3.3 SCORPIUS SUB-ORBITAL DEMONSTRATION
                    A microthruster array measuring one fourth the size of a penny, designed by a
                    TRW-led team for use on micro-, nano- and picosatellites, has successfully dem-
                                                                    1
                    onstrated its functionality in a live fire test aboard a Scorpius sub-orbital sounding
                    rocket built by Microcosm on March 9, 2000. Individual MEMS thrusters, each a
                    poppy seed-sized cell fueled with lead styphnate propellant, fired more than 20
                    times at 1-sec intervals during the test staged at the White Sands Missile Range.
                                          4                   4
                    Each thruster delivered 10  newton sec of impulse.
                    1.3.4 MEPSI

                    The series of MEMS-based Pico Sat Inspector (MEPSI) space flight experi-
                    ments demonstrated the capability to store a miniature (less than 1 kg) inspector
                    (PICOSAT) agent that could be released upon command to conduct surveillance
                    of the host spacecraft and share collected data with a dedicated ground station.
                    The DoD has approved a series of spiral development flights (preflights) leading
                    up to a final flight that will perform the full MEPSI mission. The first iteration
                    of the MEPSI PICOSAT was built and flown on STS-113 mission in December
                    2002.
                       All MEPSI PICOSATs are 4   4   5 in. cube-shaped satellites launched in
                    tethered pairs from a special PICOSAT launcher that is installed on the Space
                    Shuttle, an expandable launch vehicle (ELV) or a host satellite. The launcher that
                    will be used for STS/PICO2 was qualified for shuttle flight during the STS-113
                    mission and will not need to be requalified. 5




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