Preheating characteristics of H2O2 monopropellant thruster using manganese oxide catalyst
Author:
Funder
National Research Foundation of Korea
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference23 articles.
1. Chugging instability of H2O2 monopropellant thrusters with reactor aspect ratio and pressures;An;J. Propuls. Power,2011
2. Scaling and evaluation of Pt/Al2O3 catalytic reactor for hydrogen peroxide monopropellant thruster;An;J. Propuls. Power,2009
3. Comparison of catalyst support between monolith and pellet in hydrogen peroxide thrusters;An;J. Propuls. Power,2010
4. Design and development of ionic liquid dual-mode spacecraft propellants;Berg,2012
5. Evaluation of HAN-based propellant blends;Dieter,2003
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