The preliminary design and status of a hydrazine milliNewton thruster development
Author:
Affiliation:
1. JPL, Pasadena, CA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1999-2596
Reference5 articles.
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3. Geometrical characterization and performance optimization of monopropellant thruster injector;The Egyptian Journal of Remote Sensing and Space Science;2012-12
4. Catalytic Ignition in Hydrogen Peroxide-based Space Propulsion Systems;48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2012-07-30
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