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Osiander / MEMS and microstructures in Aerospace applications  DK3181_c011 Final Proof page 245 1.9.2005 12:31pm




                    Micropropulsion Technologies                                    245


                                                  JET

                       Transmission Mode Illumination
                       Protects optics
                       Improves device geometry

                                                                   140 µm
                                                                    hole
                                                                             ~
                                                           Ablatant         t  ~ 160 µm
                                                                            1
                                                                              ~
                              Transparent substrate, e.g.,  acetate film, is not penetrated  t 2  ~ 80 µm
                                        Fast lenses




                                            Rep-pulsed laser diode
                                             (1−5 W peak power)
                    FIGURE 11.11 LAT principle of operation — transmission mode. (Source: Photonics
                    Associates.)

                    side of the tape to high temperature, producing a miniature ablation jet. Part of the
                    acetate substrate is also ablated. A plasma is produced and the pressure inside the
                    plasma drives the exhaust, which produces thrust.
                       The mLPT can operate pulsed or CW, and power density on target is optically
                    variable in an instant, so operating parameters can be adjusted to throttle the output
                    of the thruster. Materials explored for the transparent substrate include cellulose
                    acetate, PET, and Kaptone polyimide resin. For the ablatant, over 160 materials
                    have been studied. Many of these were so-called ‘‘designer materials’’ created
                    especially for this application.
                       The thrust produced by this system depends on the so-called ablation efficiency,
                    which describes the ratio of kinetic energy and laser energy.
                       This efficiency is defined as:
                                                h AB  ¼ C m v E                  (11:16)


                    where v E is the exhaust velocity and C m as calculated, using the following equation,
                    is the so-called coupling coefficient, which depends on the laser input and the
                    material ablated through:

                                                     c 9=16   mN
                                        C m ¼ 58:3     p ffiffiffi
                                                 A 1=8 (Il t) 1=4  W             (11:17)
                                                   2
                                        c ¼ (A=2)(Z (Z þ 1)) 1=3
                    where A is the atomic mass number of material, Z the average charge state, I the
                    laser intensity, l the laser wavelength, and t the pulse duration.




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