The 35L Propellant Tank from Antrix Corporation Limited is a Spacecraft and Satellite Propellant Tank with a nominal internal volume of 35 L and a residual volume of 250cc. This propellant tank has an operating pressure of 24 bar and a burst pressure of 96 bar. It has a proof pressure of 36 bar with a maximum propellant flow rate of 50 cc/s. The propellant tank is constructed using Ti-6Al-4V commercially pure titanium and SS-304L. It supports 16 holes of 5.5 Dia on 214 PCD interface and has a dry mass of 7 kg.
