A note on wire ignition in combustion-heated drivers for shock-tunnel application
Wire ignition in combustion-heated drivers for shock tunnel application
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Wire ignition in combustion-heated drivers for shock tunnel application
Spontaneous ignition and reaction characteristics of hypergolic propellant pair in low pressure and temperature environment, specifically hydrazine fuel and nitrogen tetroxide atmosphere
Ignition delay time of hydrazine nitrogen tetroxide system in presence of various additives
Solutions to hydrogen-oxygen reaction ignition kinetics
Ignition characteristics of evaporating fuel evaluated by similarity theory and mathematical model analysis
Breaking electric contacts for ignition systems
Safety procedures for handling IMP retrorocket and igniter
Solid rocket combustion chamber overpressures due to interference from aft-end ignition rocket
Analytic solution for ignition kinetics of dry carbon monoxide-oxygen reaction
Ignition temperatures of powdered metals in simulated atmospheres of Venus and Mars suggest potential chemical energy sources
Analytic solution for ignition kinetics of dry carbon monoxide-oxygen reaction obtained, assuming initiation reaction followed by chain-branching steps
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Applicability of low temperature ignition method for determining carbon in alkali metals
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Vacuum-ignition phenomena in Apollo rocket engine when oriented in upward-firing attitude
A current from a sustaining power supply flows through the mercury vapor lamp and, as there are no resistors in series with this supply, the power is efficiently used. This high voltage igniting device protects the transistorized high current, low voltage power supply.
High voltage, low current pulse in series with arc power supply efficiently ignites a carbon arc. The easily and economically produced circuit is useful with arc burners and searchlights and with plasma jets.