ISRO's Semi-Cryogenic Engine Development: Enhancing LVM3 Payload Capacity
| Aspect | Details |
|---|---|
| Organization | ISRO ( Indian Space Research Organisation) |
| Lead Centre | Liquid Propulsion Systems Centre (LPSC) |
| Supporting Centres | Other launch vehicle centers |
| Objective | Develop a semi-cryogenic propulsion system to enhance payload capacity |
| Target Launch Vehicle | Launch Vehicle Mark-3 (LVM3) and future launch vehicles |
| Thrust of Semi-Cryogenic Engine | 2,000 kN |
| Propellant Combination | Liquid Oxygen (LOX) and Kerosene |
| Major Accomplishment | Successful ignition of semi-cryo pre-burner |
| Testing Location | Isro Propulsion Complex (IPRC), Mahendragiri |
| Ignition Fuel Combination | Triethyle Alumnide and Triethyle Boron |
| Fuel Developer | Vikram Sarabhai Space Centre (VSSC) |
| Next Steps | Develop and test engine powerhead test article and fully integrated engine |
| Semi-Cryo Stage Development | Propellant loading of 120 tons |