Abstract: The working process of an Oxygen control valve for the pre-burner of a liquid propellant staged combustion rocket engine is analyzed, according its structure. The model of control valve is ...

Abstract: This paper presents an optimal control strategy which includes the optimal switching instants and the optimal control input to solve the optimal control problem of aero-engine system with ...

The 8H and 4H modules allow HBUS devices to be star-wired back to a secure controller cabinet. Star-wiring can remove the risk of one faulty connection taking down all downstream devices as on a daisy ...

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