Designed and developmed to power the Pilotless Target Aircraft, LAKSHYA. This engine is a single shaft, Light weight, low cost turbojet engine, which is remotely controlled during flight.
Main Characteristics
| Main Characteristics | |
|---|---|
| Maximum Diameter (m) | 0.33 |
| Length (m) | 1.38 |
| Weight (kg) | 69 |
| Thrust(kg) | 380 |
| Specific Fuel Consumption (kg / deN-hr) | 1.20 |
Features
- 4-stage axil compressor driven by an axial turbine, annular combustor, and power control unit.
- Digital electronic fuel control system
- Develops 380 kg thrust
Can be refurbished after land/sea recovery
