The IFM 350 Nano Thruster - Introducing very high Δv Capabilities for Nanosats and Cubesats
Author:
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2016-5044
Reference8 articles.
1. Development of an Indium mN-FEEP Thruster
2. Consolidation of milli-Newton FEEP Thruster Technology based on Porous Tungsten Multiemitters
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