Indigenous design and development: Engineered entirely in India by RAGHU VAMSI team of skilled engineers and supported by IIT, Hyderabad. A great demonstration of the potential of Industry Academia partnership.
– Self-reliance and autonomy: By reducing reliance on imported technologies, components, and expertise, the Micro Turbojet Engine contributes to India’s goal of achieving self-sufficiency in critical sectors, bolstering national security and economic resilience.
Excellent Thrust to Weight Ratio. || Light weight || 25 hours maintenance cycle.
Main applications are for UAVs, APUs, range extenders and missile systems . Customizable ECU parameters for integration with different equipment and start methods.
PARAMETERS | METRIC | PARAMETERS | METRIC |
---|---|---|---|
Nominal Thrust | 240 N | Exhaust Gas Temp | 550 – 690 Degree Centigrade |
Idle Thrust | 12 N | Fuel Consumption | 790 grams/min at max RPM |
Idle RPM | 35,000 | Fuel Type | Jet – A1/ Kerosene/ Diesel + 5% oil |
Maximum RPM | 110,000 | ||
Speed Range | 0.9 M |
DIMENSIONS | METRIC | OPERATING ENVELOPE | METRIC |
---|---|---|---|
Outer Diameter | 121 mm | Max. Operating altitude | 8000 m |
Length | 325 mm | Max. Starting altitude | 3000 m |
Weight | 1800 grams | Speed range for startup | 0 to 0.15M |
Temperature starting range | -20 ~ +50 0C |
The engine comes with ECU and GSU with inbuilt EGT sensor, solid valves and only one integrated fitting (FASTO) to the engine. The package also includes Engine mount set, Fuel pump set, Fuel tube, Fuel filter, Cut-off valve, FOD screen, Electronic cables and a complete instruction manual.