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                   264                       MEMS and Microstructures in Aerospace Applications


                   11.4.1 PRINCIPLE OF OPERATION
                   The microsatellite obtains a thrust as the radioisotope emits the alpha or beta, or
                   both particles.
                     The thrust produced can be calculated as:
                                                              r ffiffiffiffiffiffi
                                                                2E
                                                         10
                                       T ¼ _ mmv ¼ (A(3:7   10 )m P )           (11:33)
                                                                m P
                   with A representing the radioisotope activity in C i , m P standing for the particle mass
                   and E being the kinetic energy of the particle.

                   11.4.2 SYSTEM REQUIREMENTS
                   The system itself is extremely simple without feed mechanisms and only an
                   optional shutter. The propellant mass can be minimized by selecting the adequate
                   material. Alpha particles are easy to shield and therefore shielding should not
                   require significant amounts of additional mass. A summary of the radioisotope
                   propulsion system is shown in Table 11.11.


                   11.5 CONCLUSION
                   Ten different propulsion systems have been introduced, covering a large range of
                   requirements for small satellite propulsion. It should be mentioned that while
                   MEMS is an enabling technology for many of these systems, a significant amount
                   of research needs to be done on the systems level to approach high technical
                   readiness levels (TRL) that will lead to use of these technologies in upcoming
                   missions. In September 2003, DARPA had initiated an effort to push MEMS
                   technology into a different venue — that of high power electric propulsion. Field
                   effect thrusters like colloids and FEEP systems with power levels of up to 1 kW



                   TABLE 11.11
                   Radioisotope Propulsion Characteristics
                                        6
                                    3.9.10 sec             5.67 MeV alpha particles
                   I sp
                   I-bit (if pulsed)  1.55.10  4  mNsec    Pulse rate is limited by valve — assume
                                                            1 KHz MEMS valve   1 msec
                   Rep. rate (if pulsed)  1 kHz            1 kHz MEMS valve is an option
                   Power            0 W—no valve/1 mW with valve 0 W required to generate particles
                   Thrust           0.155 mN               100 Curie of Pu-238
                   Thrust or power  Infinity mN/W (0 valve),  Without valve power consumption is zero,
                                    155 mN/W (with valve)  With valve operating at 1 mW
                   Impulse or prop.  1.58   10  5  Nsec/g
                   Total impulse/sys.-mass 428 Nsec/2g
                   Current system mass  2 g (with valve)






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