Dependence of Pellet Shape and Size on Pressure Drop in H2O2 Thrusters
Author:
Affiliation:
1. Aerodynamics and Flight Mechanics Group, University of Southampton, Southampton SO17 1BJ, United Kingdom
2. DELTACAT Ltd., Fareham PO16 7BB, United Kingdom
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.B35072
Reference36 articles.
1. Capabilities of hydrogen peroxide catalyst beds
2. Catalyst bed instability within the USFE H2O2/JP-8 rocket engine
3. One-Dimensional Modeling of Catalyzed H2O2 Decomposition in Microchannel Flows
4. Modeling of Catalyzed Hydrogen Peroxide Decomposition in Slender Microchannels with Arrhenius Kinetics
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