Page 274 - MEMS and Microstructures in Aerospace Applications

Osiander / MEMS and microstructures in Aerospace applications DK3181_c011 Final Proof page 265 1.9.2005 12:31pm

Micropropulsion Technologies 265

based on MEMS technology have been proposed. In that case, MEMS technology is
not used to minimize the propulsion system, but to allow for the manufacturing of
large arrays in which each individual emitter operates at a highly efficient low level
of emission current.
Research on MEMS propulsion is advancing quickly, and it should not be
limited to the thrusters but include PPU and interface development as well to
make ‘‘intelligent dust’’ a possibility in the near future.

REFERENCES
1. M. Birkan, Formation Flying and Micro-Propulsion Workshop, Lancaster, CA, October
1998.
2. J. Dunning and J. Sankovic, in 35th Joint Propulsion Conference, Los Angeles, CA,
1999. AIAA-99-2161.
3. R.A. Spores and M. Birkan, in 35th Joint Propulsion Conference, Los Angeles, CA,
1999. AIAA paper 99–2162.
4. M. Birkan, AAAF Propulsion Symposium, paper 16–355, 2002.
5. K.E. Tsiolkovsky. Issledovanie Mirovykh Prostransty Reaktivnymi Priborami (Explor-
ation of Space with Rocket Devices). Naootchnoye Obozreniye (Scientific Review),
1903.
6. R. Raju, B.P. Pandey, and S. Roy, Finite Element Model of Fluid Flow inside a Micro
Thruster, AIAA paper 2002–5733, Nanotech, 2002.
7. J. Hammel, Development of an Unstructured 3-D Direct Simulation Monte Carlo/
Partice-In-Cell Code and the Simulation of Microthruster Flows, MS thesis, Worcester
Polytechnic Institute, 2002.
8. J. Mueller, in Micropropulsion for small spacecraft, M.M. Micci and A.D. Ketsdever,
(eds) Progress in Astronautics and Aeronautics, vol. 187, p. 45, 2000.
9. http://www.grc.nasa.gov/WWW/RT1997/6000/6910curran.htm.
10. P. Gessini and G. Paccani, Ablative Pulsed Plasma Thruster System Optimization for
Microsatellites, IEPC paper 01–182, 27th IEPC, 2001
11. M. Keidar, I. Boyd, E. Antonsen, and G. Spanjers, Progress in Development of Modeling
Capabilities for a Micro-Pulsed Plasma Thruster, 39th Joint Propulsion Conference,
Huntsville, AL, 2003. AIAA paper 2003–5166.
12. J. Ziemer, Laser Ablation Microthruster Technology, 33rd Plasmadynamics and Lasers
Conference, Maui, HI, 2002, AIAA paper 2002–2153.
13. J. Ziemer, Performance Scaling of Gas-Fed Pulsed Plasma Thrusters, PhD thesis, Prince-
ton University, 2001.
14. C. Zakrzwski, S. Benson, P. Sanneman, and A. Hoskins, On-Orbit Testing of the EO-1
Pulsed Plasma Thruster, AIAA paper 2002.
15. F. Rysanek and R. Burton Performance and Heat Loss of a Coaxial Teflon Pulsed Plasma
Thruster, IEPC paper 01–151, 27th IEPC, 2001.
16. www.busek.com
17. J. Schein, A. Anders, R. Binder, M. Krishnan, J.E. Polk, N. Qi, and J. Ziemer, Inductive
energy storage driven vacuum arc thruster, Review of Scientific Instruments, vol. 72, no.
3, February 2002.
18. J. Schein, N. Qi, R. Binder, M. Krishnan, J.K. Ziemer, J.E. Polk, and A. Anders, Low
Mass Vacuum Arc Thruster System for Station Keeping Missions, IEPC paper 01–228,
27th IEPC, 2001.

© 2006 by Taylor & Francis Group, LLC