Heat transfer studies of solid rocket igniters quarterly progress report no. 3
Heat transfer of solid rocket igniters - flow visualization tests, copper tube firing, and radiant heat transfer analysis
FLOW VISUALIZATION↗
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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 physical criterion for metal ignition.
Ignition temperatures of magnesium ribbon and aluminum wire samples electrically heated in argon-oxygen-carbon dioxide-water vapor mixtures
COMBUSTION TEMPERATURE↗
Preliminary experiments on ignition in carbon dioxide.
Ignition temperatures of various powdered metals in carbon dioxide may be used to determine safe handling procedures
POWDERED METAL↗
An experimental and analytical investigation of ignition and axisymmetric turbulent flame propagation in premixed hydrogen-air flows with application to supersonic combustion.
Ignition and propagation of turbulent flame front in jet flow investigated for combustible hydrogen- air mixture
GAS MIXTURE↗
Summary of literature survey of hypergolic ignition spike phenomena, phase I Final report, Apr. 8 - Dec. 31, 1965
Summary of industry survey and literature search of ignition spike phenomena in low thrust, hypergolic, liquid bipropellant rocket engines
HYPERGOLIC PROPELLANT↗
Toroidal ring prevents gas ignition at vent stack outlet
Torodial ring welded to the vent stack outlet prevents static discharges which ignite combustible gases in a venting system. The ring inhibits the flow of current by removing the cause of turbulence characteristics of a sharply defined vent exit.
Spring, T. R.↗
The ignition transient in solid propellant rocket motors.
Ignition pressure transient in solid rocket motors, examining chamber filling interval, flame propagation, heat transfer correlation, burning area, etc
TRANSIENT PRESSURE↗
A study of ignition point values of nonmetallic materials in simulated spacecraft environment.
Elastomeric materials thermostability in simulated spacecraft environment tested to obtain ignition point values
ENVIRONMENT SIMULATION↗
Ignition kinetics of the carbon monoxide-oxygen reaction.
Ignition kinetics of carbon monoxide-oxygen reaction
CHEMICAL KINETICS↗
Effect of additives on the ignition delay time of hypergolic propellants.
Additives effect on ignition delay and pressure of hypergolic hydrazine-nitrogen tetroxide propellant systems.
TIME DELAY↗
Flame spreading at elevated pressures over the surface of igniting solid propellants and propellant ingredients in oxygen/inert environments Annual report
Mathematical analysis of flame propagation at high pressures over surface of igniting solid propellants and propellant ingredients in oxygen/inert atmospheres
Magee, R. S.↗
Ignition kinetics of the carbon monoxide-oxygen reaction
Ignition kinetics of carbon monoxide-oxygen reaction
Brokaw, R. S.↗
Ignition system for the ATS rocket motor
Design and test performance of igniter system for solid propellant applications technology satellite apogee rocket motor
Lee, T. P.↗
An experimental investigation of the hypergolic ignition of some polymeric fuels with oxygen
Hypergolic ignition of polymeric fuels with oxygen
Kershner, S. D.↗
An analysis of the ignition of slot-injected gaseous hydrogen in a supersonic air stream.
Initial air boundary layer effect on ignition of slot-injected gaseous hydrogen in supersonic airstream, discussing isotherm and streamline patterns
Favin, S.↗
Minimum ignition energy determination by switchless spark discharge scheme.
Switchless spark discharge system for improved minimum ignition energy measurements of premixed gaseous combustible mixture
Cheng, D. Y.↗
Best estimate method of determining space vehicle ignition and cutoff masses.
Optimal determination of vehicle ignition and cut-off masses, discussing applications to Saturn S-4B Stage flight evaluation
Lenning, J. J.↗