Configuration
● Low-pressure Shaft: 1 stage Geared FAN + 2 stages IPC + Gear Reducer + 1 stage LPT;
● High-pressure shaft: 1 stage centrifugal compressor + 1 stage HPT;
● Combustion Chamber: Annular Reverse-flow;
● Exhaust: Petal Mixer, Outer-inner Mix.
Application
Characteristics
Take-off Thrust: 560 kg
Take-off SFC: 0.42 kg/ (kgf.h)
Bypass Ratio: 4.33
Total Pressure Ratio: 18.06
Gear Transmission Ratio: 2.15
Turbine Inlet Temp: 1319k
Thrust-weight Ratio: 4.4
Length: 1706 mm
height: 651 mm
Dry Weight: 124 kg
Representative Specifications (indicative)
| Parameter | Value / Range | Notes |
|---|---|---|
| Engine Type | Turbofan | Single-shaft or dual-spool configuration depending on variant |
| Thrust | ~5,000–5,500 N | Approximate maximum take-off thrust |
| Bypass Ratio | 1.2–1.5 | Low bypass for high-speed tactical performance |
| Overall Pressure Ratio | ~12–15 | Optimized for fuel efficiency and reliability |
| Specific Fuel Consumption | ~0.8 kg/N·h | Indicative, depending on flight conditions |
| Engine Weight | ~120–140 kg | Compact and lightweight design |
| Diameter | ~0.45 m | Suitable for light tactical aircraft and UAVs |
| Length | ~1.2 m | Approximate overall length |
| Operational Altitude | 0–15,000 m | Capable of low-to-high altitude operations |
| Temperature Range | -40°C to +55°C | Operates under harsh environmental conditions |
| Maintenance Interval | ~300–500 flight hours | Indicative, depending on usage and operational conditions |
Key Features
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High Thrust-to-Weight Ratio: Delivers efficient propulsion for tactical and high-speed flight.
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Fuel Efficiency: Optimized turbine and compressor design reduces fuel consumption during sustained operation.
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Compact & Lightweight: Modular architecture allows for easy integration into multiple aircraft platforms.
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Reliable Operation: Designed for continuous and safe operation under diverse environmental conditions.
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Low Maintenance: Extended service intervals with simplified inspection procedures.
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Advanced Materials: Utilizes high-temperature alloys for turbine blades and critical components for durability.
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Flexible Integration: Compatible with fixed-wing aircraft, UAVs, and trainer jets.
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Digital Engine Control (Optional): Can be equipped with FADEC (Full Authority Digital Engine Control) for precise performance management.
