A performance evaluation of MEMS-based micronozzles
Author:
Affiliation:
1. MIT, Cambridge, MA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1997-3169
Reference15 articles.
1. Janson, S. W. "The On-Orbit Role of Electric Propulsion,"AIAA Paper 93-2220, June 1993.
2. Figure 11: Nozzleflow rates forvarying geometries exhausting to an exit chamber of 5torr. Throat diameters range from 30-31 microns.
3. Electron-beam studies of viscous flow in supersonic nozzles
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