The VINCI from ArianeGroup is a Satellite Launch Vehicle Engine with Height 3.22 m, Nozzle Outlet Diameter 1.84 m, Propellant Flow Rate 24.20 / 4.40 to 34.11 /5.59 Kg/s, Specific Impulse 457.2 to 458.2 sec, Vacuum Thrust 130 to 180 kN. More details for VINCI can be seen below.