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                    Micropropulsion Technologies                                    253



                          TABLE 11.6
                          Performance Characteristics for Water (Micro) Resistojet

                          I sp                         152 s (water)    100 s
                          Power                        100 W            3 W
                          Thrust                       45 mN            500 mN
                          Thrust or power              450 mN/W          150 mN/W
                          Impulse or prop.             1.5 Ns/g          1 Ns/g
                          Feed mechan.                 Yes              Yes
                          Current system dry mass      1240 g            50 g
                          (includes PPU, valve, tank, etc.)





                       Current micro-resistojets are a few centimeters in length. A pure MEMS
                    resistojet is the vaporizing liquid microthruster, which is described in the next
                    section, or the Free Molecular Resistojet from AFRL. A summary of the water
                    (micro) resistojet is shown in Table 11.6.


                    11.2.7 VAPORIZING LIQUID MICROTHRUSTER
                    One resistojet concept that is built on MEMS technology is the vaporizing liquid
                                                               26,38,39
                    Microthruster (VLM) developed at the NASA JPL.   This microfabricated
                    thruster device is primarily targeted for use in constellations of microspacecraft to
                    serve as attitude control thrusters. The thruster vaporizes a suitable propellant, such
                    as water, ammonia, or others stored compactly in its liquid phase, on demand for
                    thrust generation. While the use of valves for gaseous propellants in MEMS devices
                    has been problematic in the past due to unavoidable leakage of the liquid, propellant
                    storage of the VLM reduces these concerns and, as already mentioned, reduces
                    system mass and size requirements over high-pressure gaseous storage. The thruster
                    chip itself is fabricated using MEMS technologies into silicon material and will
                    ultimately be tightly integrated with a micropiezovalve to form a very compact
                    thruster module.

                    11.2.7.1  Principle of Operation
                    The VLM is a pure resistojet, similar to the design by Surrey. Liquid propellants,
                    like water, are pressure-fed between heater strips, vaporized, and expanded through
                    a micronozzle, producing thrust.
                       To enable MEMS fabrication, innovative designs had to be employed. Due to
                    the short distances, sufficient thermal insulation is necessary to limit power con-
                    sumption to the small heating section. The current VLM concept design is T-shaped
                    to thermally isolate the heater section from the bulk of the chip as shown in Figure
                    11.16. Figure 11.17 shows the laminate of three chips. The two outermost layers





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