NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Microfluidic Flame BarrierPropellants flow through specialized mechanical hardware that is designed for effective and safe ignition and sustained combustion of the propellants. By integrating a micro-fluidic porous media element between a propellant feed source and the combustion chamber, an effective and reliable propellant injector head may be implemented that is capable of withstanding transient combustion and detonation waves that commonly occur during an ignition event. The micro-fluidic porous media element is of specified porosity or porosity gradient selected to be appropriate for a given propellant. Additionally the propellant injector head design integrates a spark ignition mechanism that withstands extremely hot running conditions without noticeable spark mechanism degradation.
Document ID
20150003140
Acquisition Source
Jet Propulsion Laboratory
Document Type
Other - Patent
Authors
Mungas, Gregory S.
Fisher, David J.
Mungas, Christopher
Date Acquired
March 18, 2015
Publication Date
November 5, 2013
Subject Category
Fluid Mechanics And Thermodynamics
Funding Number(s)
CONTRACT_GRANT: 1265181
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-Patent-8,572,946
Patent Application
US-Patent-Appl-SN-13/549,027
No Preview Available