It is a special design combustor unit for the high presser and high-temperature operation. Its cooling system has properly designed for long duration operation, It has been running long period in IIT (Chennai) and ISRO Centers.
Project Completed
- Turbocam TEST RIG – 2020
- DRDO (GTRE) TEST RIG – 2021
- TEL (Turbo Energy LTD) Natural GAS Test Rig – 2021
Technical Specification
| COMBUSTOR ASSEMBLE | 2.5 Kg per Second | 1 Kg per Second |
| Mass Flow rate | 2.5 kg /Sec | 1 kg /Sec |
| Operating pressure Range (Absolute) | 23-Bar to 35-Bar | 10-Bar to 25-Bar |
| Exit Temperature | 800 K to 1200 K | 800 K to 1200 K |
| Fuel Tank | ||
| Tank Capacity | 30-Litter | 20-Litter |
| Tank pressure (Absolute) | 50-Bar | 25-Bar |
| Flow meter – Range | 0 to 30 –ml/Sec | 0 to 20 –ml/Sec |
| Fuel controller valve | Manual operating needle valve | Manual operating needle valve |