FIELD: engines and pumps.
SUBSTANCE: gaseous hydrogen and oxygen thruster consisting of an engine head, a fuel spark plug, a system of fuel supply to a combustion chamber and of internal combustion chamber cooling, while the slot nozzle is installed to supply an oxidizer into the combustion chamber and direct the oxidizer to the motor axis.
EFFECT: invention promotes intensive mixing of hydrogen and oxygen and their more complete combustion.
1 dwg
Authors
Dates
2017-07-03—Published
2016-10-03—Filed