Turbofan Engines
F125 Turbofan Engine
The F125 is a high-performance, reliable, modular engine designed specifically for today’s lightweight fighter/attack aircraft and advanced trainers.
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The F125 design provides state-of-the-art performance and operability. The low-bypass ratio/high-pressure ratio design results in excellent altitude and Mach number lapse rates without sacrificing specific fuel consumption (SFC). The F125 also boasts more thrust and more significant weight savings than other engines in its class.
The F125 turbofan engine is produced by the International Turbine Engine Company (ITEC), LLC, a partnership of Honeywell and AIDC.
Physical
- Weight
- 1360 lbs
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- Compatible Platform
- AIDC F-CK1 (IDF)
Power and Electrical
- Takeoff Thrust
- 6025/9250 lbs
Performance
- Key Benefits
- Afterburning design
- Dual Channel FADEC
- Ease of maintenance
- F125 is equipped with an afterburner, which provides extra thrust for supersonic speeds, making it suitable for frontline combat aircraft.
- High durability
- High platform availability
- High reliability
- Higher payload available to aircraft
- Lower maintenance costs
- Modular engine design
Physical
- Weight
- 1360 lbs
Filter
- Compatible Platform
- AIDC F-CK1 (IDF)
Power and Electrical
- Takeoff Thrust
- 6025/9250 lbs
Performance
- Key Benefits
- Afterburning design
- Dual Channel FADEC
- Ease of maintenance
- F125 is equipped with an afterburner, which provides extra thrust for supersonic speeds, making it suitable for frontline combat aircraft.
- High durability
- High platform availability
- High reliability
- Higher payload available to aircraft
- Lower maintenance costs
- Modular engine design
- Weight : 1360 lbs
- Compatible Platform : AIDC F-CK1 (IDF)
- Takeoff Thrust : 6025/9250 lbs
- Key Benefits : Afterburning design|Dual Channel FADEC|Ease of maintenance|F125 is equipped with an afterburner, which provides extra thrust for supersonic speeds, making it suitable for frontline combat aircraft.|High durability|High platform availability|High reliability|Higher payload available to aircraft|Lower maintenance costs|Modular engine design
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