The Redundant Engine Control Valve (0.05 hp) from Moog is a Launch Vehicle Rotary Actuator with an actuator mass of 7.25 Kg. It has a horsepower of 0.05 Hp and a power point of 60 in/lbf (at 360 deg/sec). This flight-proven electromechanical actuator requires a DC supply of 28 V and has a stroke of 100 deg. It has provided thrust vector control (TVC) for several launch vehicles such as Antares, Delta IV, Centaur, and Vega.
