Methodology for Geometric Optimization and Sizing for Subnewton Monopropellant Catalyst Beds
Author:
Affiliation:
1. University of Southampton, Southampton, England SO17 1BJ, United Kingdom
2. Surrey Satellite Technology, Ltd., Guildford, England GU2 7YE, United Kingdom
Funder
University of Southampton
Surrey Satellite Technology Ltd.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.B38083
Reference23 articles.
1. The technological and commercial expansion of electric propulsion
2. Microcooling Channel Effect on a Monopropellant Microelectromechanical System Thruster Performance
3. MEMS-based satellite micropropulsion via catalyzed hydrogen peroxide decomposition
4. Design, Fabrication, and Test of a Microelectromechanical-System-Based Millinewton-Level Hydrazine Thruster
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