作者: Gregory S. Mungas , David J. Fisher , Christopher Mungas
DOI:
关键词: Combustion chamber 、 Ignition system 、 Detonation 、 Propellant 、 Porous medium 、 Combustion 、 Composite material 、 Nuclear engineering 、 Materials science 、 Monopropellant 、 Injector
摘要: Propellants flow through specialized mechanical hardware that is designed for effective and safe ignition sustained combustion of the propellants. By integrating a micro-fluidic porous media element between propellant feed source chamber, an reliable injector head may be implemented capable withstanding transient detonation waves commonly occur during event. The specified porosity or gradient selected to appropriate given propellant. Additionally design integrates spark mechanism withstands extremely hot running conditions without noticeable degradation.