ATAL (Advanced Tabletop Aeroengine Lab)
DET TJ – 200
ATAL is a first of its kind micro gas turbine with 200N thrust which can be used for research applications. This fully instrumented engine is designed to support advanced research initiatives in the area of gas turbine development and research. Combining precision engineering with innovation, Dheya micro gas turbine offers unparalleled performance and data-rich capabilities for various research applications.
Technical Specifications
- Maximum Thrust: 180N @ 122000 RPM
- Idle Speed: 40000 RPM
- Pressure Ratio: 3.8
- Exhaust Gas Temperature: <750 C
- Fuel Consumption: 500 ml/min
- Engine Diameter: 111mm
- Engine Length: 240mm
- Engine Weight: 1.8 kgs
Applications
Images
Engine
