| 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 |
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.
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