ISRO, through the Liquid Propulsion Systems Centre (LPSC) with support from other launch vehicle centers, is advancing the development of a semi-cryogenic propulsion system. This system aims to enhance the payload capacity of Launch Vehicle Mark-3 (LVM3) and future launch vehicles by utilizing a 2,000 kN thrust semi-cryogenic engine powered by a combination of liquid oxygen (LOX) and kerosene.
