RELATIVE IGNITABILITY OF TYPICAL SOLID PROPELLANTS WITH CHLORINE TRIFLUORIDE
Relative ignitability of solid propellants exposed to chlorine trifluoride
CHLORINE TRIFLUORIDE↗
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Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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A SHOCK TUBE OF IGNITION OF METHANE-OXYGEN MIXTURES
Shock tube ignition of methane-oxygen mixtures
OXYGEN↗
EFFECT OF ANTIKNOCKS ON FLAME PROPAGATION IN A SPARK IGNITION ENGINE
Effect of antiknock compounds on combustion processes and flame propagation in spark ignition internal combustion engine
SPARK IGNITION↗
Baker-nunn photography of the syncom ii fourth-stage ignition
Baker-Nunn photography of Syncom II fourth stage ignition, duration, and burnout
BURNOUT↗
Analytic solutionsto the ignition kinetics of the hydrogen-oxygen reaction
Analytic solutions to ignition kinetics of hydrogen-oxygen reaction
IGNITION↗
Effectiveness of various agents for suppressing ignition of rp-1 and hydrogen under flow conditions
Inert gases, halogenated hydrocarbons for suppressing ignition of oxygen mixtures with hydrogen and RP-1 under conditions of turbulent flow
INERT GAS↗
Experimental results for thermal ignition of hydrogen in a supersonic viscous flow technical report no. 404
Wind tunnel tests for determining ignition characteristics of hydrogen vented from supersonic launch vehicle
SUPERSONIC WIND TUNNEL↗
Analytic Solutions to the Ignition Kinetics of the Hydrogen-Oxygen Reaction
Analytic solutions to ignition kinetics of hydrogen-oxygen reaction
OXYGEN↗
A note on wire ignition in combustion-heated drivers for shock-tunnel application
Wire ignition in combustion-heated drivers for shock tunnel application
WIRE↗
On the spontaneous ignition of hypergolic propellant systems at low pressures and temperatures.
Spontaneous ignition and reaction characteristics of hypergolic propellant pair in low pressure and temperature environment, specifically hydrazine fuel and nitrogen tetroxide atmosphere
NITROGEN OXIDE↗
Modification of the hydrazine-nitrogen tetroxide ignition delay.
Ignition delay time of hydrazine nitrogen tetroxide system in presence of various additives
NITROGEN OXIDE↗
Analytic solutions to the ignition kinetics of the hydrogen-oxygen reaction.
Solutions to hydrogen-oxygen reaction ignition kinetics
OXYGEN↗
Ignition of an evaporating fuel in a hot, stagnant gas containing an oxidizer.
Ignition characteristics of evaporating fuel evaluated by similarity theory and mathematical model analysis
IGNITION LIMIT↗
Investigation of breaking contacts for ignition assemblies
Breaking electric contacts for ignition systems
IGNITION SYSTEM↗
IMP D TE-M-458 retromotor and igniter safety and handling plan
Safety procedures for handling IMP retrorocket and igniter
IGNITER↗
Compressed-air model investigation of solid rocket overpressures due to interference from aft-end ignition rocket
Solid rocket combustion chamber overpressures due to interference from aft-end ignition rocket
ROCKET BOOSTER↗
Ignition kinetics of carbon monoxide - oxygen reaction
Analytic solution for ignition kinetics of dry carbon monoxide-oxygen reaction
OXYGEN RECOMBINATION↗
Ignition and combustion of powdered metals in the atmospheres of Venus, earth, and Mars.
Ignition temperatures of powdered metals in simulated atmospheres of Venus and Mars suggest potential chemical energy sources
POWDERED METAL↗