ISRO develops a 2,000 kN semi-cryogenic engine using LOX Kerosene propellant at IPRC, Mahendragiri. LPSC leads with ISRO support, achieving pre-burner ignition test at SIET and PRLD. Triethyle Alumnide is used for ignition.
ISRO developing semi-cryogenic engine working on liquid oxygen kerosene
