Ignition system for the ATS rocket motor
Design and test performance of igniter system for solid propellant applications technology satellite apogee rocket motor
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Design and test performance of igniter system for solid propellant applications technology satellite apogee rocket motor
Hypergolic ignition of polymeric fuels with oxygen
Initial air boundary layer effect on ignition of slot-injected gaseous hydrogen in supersonic airstream, discussing isotherm and streamline patterns
Switchless spark discharge system for improved minimum ignition energy measurements of premixed gaseous combustible mixture
Optimal determination of vehicle ignition and cut-off masses, discussing applications to Saturn S-4B Stage flight evaluation
Spectrographic method determines individual stainless steel components in molten bismuth-42 w/o tin eutectic to determine the solubility of Type 304 stainless steels. It utilizes the high sensitivity and precision of the spark-ignited, low-voltage ac-arc excitation of samples rendered homogeneous by dissolution.
Evaluation of ignition mechanisms for spacecraft materials in simulated spacecraft cabin atmospheres
Ignition mechanism of hydrazine-nitrogen dioxide hypergolic propellant system
Vacuum ignition characteristics of Flox-diborane and oxygen difluoride-diborane
Minimum electromagnetic field intensity required to ignite hydrogen-air mixture
Effect of fuel injection on ignition process of hydrazine-nitric acid system
Engine design and operating parameters studied for effects on rocket engine ignition and popping
Vacuum ignition characteristics of rocket engine using oxygen difluoride-diborane propellant
Catalytic ignition system for promoting hydrogen, oxygen combustion
Liquid hydrazine ignition by nitrogen tetroxide gas based on stagnation flow principle, presenting threshold measurements
Reasonance induced in stoichiometric mixtures of gaseous hydrogen-oxygen produces temperatures /over 1100 deg F/ high enough to cause ignition. Resonance tube phenomenon occurs when high pressure gas is forced through sonic or supersonic nozzle into short cavity. Various applications for the phenomenon are discussed.
Atmospheric selection and gravity effects on burning rate and ignition temperature
Theoretical analysis of ignition mechanisms and quantitative analysis of vapor phase reaction products of dimethylhydrazines with nitrogen dioxide