 With a mass of 1370 kg at launch, AMOS-2 incorporated a 400 newton Liquid Apogee Boost Motor (ABM) and fourteen 10 newton Reaction Control Thrusters for raising the satellite's orbit from Geostationary Transfer orbit to its final geostationary orbit as well as for its attitude control.It carried 450 kg of propellant (monomethyl hydrazine and MON-1).AMOS-2 measures 11.5 m in length in its final in-orbit configuration.