The T11-0 from Orbital Propulsion Centre is a Spacecraft & Satellite Propellant Tank with a net tank volume of 218 L and a maximum expected operating pressure of 22 bar. This propellant tank is compatible with MON propellant and pressurant gases such as helium and nitrogen. It has a proof pressure of 27.5 bar and a burst pressure of 33 bar. The tank has a spherical geometrical shape and a mass of 11 Kg. It is constructed using Ti6AI4V STA (3.7164.7) material for the pressure vessel and Ti6AI4V (3.7164.1) for the suspension/ports. The propellant tank has been used on Meteosat Second Generation satellites and is suitable for spin-stabilized spacecraft.
