ISRO has made significant progress in developing its semi-cryogenic propulsion systems by successfully igniting a pre-burner.
About
The pre-burner ignition test is part of ISRO's efforts to develop a powerful semi-cryogenic engine that will use a combination of liquid oxygen and kerosene as propellants.
This engine aims to increase the payload capacity of launch vehicles like
Start fuel ampule: Semi-cryogenic engine ignition is achieved using a start fuel ampule which uses a combination of Triethyle Alumnide and Triethyle Boron developed by Vikram Sarabhai Space Centre (VSSC).
Next steps include testing the engine power head and fully integrating the engine. Additionally, ISRO is working on developing a semi-cryo stage with 120 tons of propellant loading.
Fact Box: ISRO’s Semi-Cryogenic Engine
ISRO is developing a 2000 kN thrust semi-cryogenic engine working on an LOX Kerosene propellant combination for enhancing the payload capability of LVM3 and for future launch vehicles.
Liquid Propulsion Systems Centre (LPSC) is the lead centre for the development of semi-cryogenic propulsion systems with the support of other launch vehicle centres of ISRO.