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.↗
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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 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.↗
A resonance igniter for hydrogen-oxygen combustors
Resonance ignition technique for gaseous oxygen and hydrogen rocket propellants
Conrad, E. W.↗
Characteristics of solid propellant motor aft- end ignition
Aft-end igniter design and placement for solid propellant rocket motors avoiding overpressurization and nozzle pressure oscillations
Fitch, R. E.↗
Dynamics of arc ignition and cathode spot movement of thermionically emitting cathode surfaces
Arc ignition and cathode spot movement dynamics of thermionically emitting cathode surfaces in heat feedback plasma
Cheng, D. Y.↗
Ignition system for space shuttle auxiliary propulsion system Quarterly technical progress narrative, 29 Jun. - 27 Sep. 1970
Design of spark and plasma pulse igniters for space shuttle propulsion system
Rosenberg, S. D.↗