Thermal Diffusion Controlled Ignition of Hypergolic Gel Propellants
Author:
Affiliation:
1. Faculty of Civil and Environmental Engineering, Technion—Israel Institute of Technology, 32000 Haifa, Israel
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.B34861
Reference15 articles.
1. SuttonG. P.BiblarzO. “Rocket Propulsion Elements,” 7th ed., Wiley, New York, 2001, pp. 250–257, Chap. 7.
2. Chemical Kinetic Model for Monomethylhydrazine/Nitrogen Tetroxide Gas Phase Combustion and Hypergolic Ignition
3. Reaction Rates for Hypergolic Propellants Using Chemical Delay Times
4. An experimental study on the hypergolic ignition of hydrogen peroxide and ethanolamine
5. HYPERGOLIC REACTION MECHANISMS OF CATALYTICALLY PROMOTED FUELS WITH ROCKET GRADE HYDROGEN PEROXIDE
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