Determination of the minimum electromagnetic field intensity required to ignite a hydrogen-air gaseous mixture Interim report
Minimum electromagnetic field intensity required to ignite hydrogen-air mixture
Lester, D. L.↗
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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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Studies on the effect of fuel injection on the ignition process of the hydrazine-nitric acid system
Effect of fuel injection on ignition process of hydrazine-nitric acid system
Twardy, H.↗
Transients influencing rocket engine ignition and popping Interim report
Engine design and operating parameters studied for effects on rocket engine ignition and popping
Breen, B. P.↗
Oxygen difluoride/diborane technology vacuum ignition, phase 2 Quarterly report, 15 Jul. - 14 Oct. 1969
Vacuum ignition characteristics of rocket engine using oxygen difluoride-diborane propellant
Mistler, G. R.↗
Study of catalytic reactors for hydrogen- oxygen ignition Final progress report, 28 Aug. 1968 - 28 May 1969
Catalytic ignition system for promoting hydrogen, oxygen combustion
Kesten, A. S.↗
A basic study of ignition of hypergolic liquid propellants.
Liquid hydrazine ignition by nitrogen tetroxide gas based on stagnation flow principle, presenting threshold measurements
Breen, B. P.↗
Resonance tube igniter
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.
Conrad, E. W.↗
The effect of atmosphere selection and gravity on burning rate and ignition temperature
Atmospheric selection and gravity effects on burning rate and ignition temperature
Colombo, G. V.↗
A basic study of the ignition of hypergolic liquid propellants Final report
Theoretical analysis of ignition mechanisms and quantitative analysis of vapor phase reaction products of dimethylhydrazines with nitrogen dioxide
Breen, B. P.↗
Fundamental ignition study for material fire safety improvement Quarterly report, 1 Jan. - 31 Mar. 1970
Ignition potential of polymeric materials related to pyrolysis characteristics of material and atmospheric factors
Paciorek, K. L.↗
Rate constants from ignition studies of the H2-CO-O2 system
Rate constant determination for ignition of hydrogen carbon monoxide oxygen system
Belles, F. E.↗
Apparatus for igniting solid propellants Patent
Solid propellant ignition with hypergolic fluid injected to predetermined portions of propellant
Allen, H., Jr.↗
Computer modeling of rocket engine ignition transients Final report
Computer modeling of rocket engine ignition transients
Breen, B. P.↗
Ignition system for monopropellant combustion devices Patent
Ignition system for monopropellant combustion devices
Chilenski, J. J.↗
Ignition means for monopropellant Patent
Catalyst bed ignition system for hydrazine propellants
Evans, D. D.↗
Vacuum Ignition Characteristics of Oxygen Difluoride/diborane and Flox/diborane Final Report, 15 Jan. - 14 Dec. 1969
Vacuum ignition characteristics of oxygen difluoride diborane and FLOX diborane
Seamans, T. F.↗
Recent research on fuel injection and mixing and piloted-ignition for scramjet combustors
Fuel injection and mixing and piloted ignition in supersonic flow design principles for scramjet engine, evaluating eddy viscosity model for parallel injection
Henry, J. R.↗
Ignition of metals with ClF sub 3 and ClF sub 5 for use as spacecraft chemical heaters
Chemical heat source combined with metals ignition properties considered for spacecraft heating during Mars nighttime landing
Rhein, R. A.↗