LIQUID JET RESTARTABLE ENGINE WITH TURBO-PUMP SYSTEM OF FUEL COMPONENT SUPPLY

摘要

Disclosed is a liquid jet restartable engine with turbo-pump system of fuel component supply. The engine includes a combustion chamber, a turbo-jet unit, a gas generator, units of automation, a start system. The start system has rigidly connected to each other volumetric pumps of oxidizer and fuel with fluid power drive that by their inlet pipes are connected to outlet pipes of the pumps of turbo-pump assembly and with outlet ones – to feed lines of gas generator. At that between the output manifolds of the volumetric pumps and pumps of the turbo-pump assembly at gas generator feed line check valves are installed.