Liquid propellant rocket engines manufactured by Airbus, used primarily as apogee engines for telecommunications satellites. The chamber and throat are made of platinum alloy, using a double cone vortex injector and both film and radiative cooling.
Thrust: 96 N (21 lbf). Gross mass: 4.30 kg (9.40 lb). Specific impulse: 321 s. Height: 0.67 m (2.19 ft). Diameter: 0.32 m (1.04 ft).