Assessment of Catalysts for Hydrogen-Peroxide-Based Thrusters in a Flow Reactor
Author:
Affiliation:
1. Institute for Energy Systems and Thermodynamics, Vienna University of Technology, 1040 Vienna, Austria
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.B34615
Reference30 articles.
1. PonzoJ. “Small Envelope, High Flux 90% Hydrogen Peroxide Catalyst Bed,” AIAA Paper 2003-4622, 2003.
2. Chemical and Material Science Department/Rocketdyne, Hydrogen Peroxide Handbook “Hydrogen Peroxide Handbook,” AFRPL TR-67-144, 1967.
3. X-15 propulsion system
4. Development of Hydrogen Peroxide Monopropellant Rockets
5. SiscoJ. C. “Autoignition of Kerosene by Decomposed Hydrogen Peroxide in a Dump Combustor Configuration,” Master Thesis, Purdue Univ., West Lafayette, IN, 2003.
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