Is a single shaft turbojet engine, which consists of:
This engine has a simple design, low cost, and high thrust to weight ratio. The speed control of the engine is hydro-pneumatic. The lifetime of the engine is 20 hours or 50 starts.
| SPECIFICATIONS | |
| Engine Type | Mini Jet |
| Thrust | 345 daN |
| CPR | 3.65 |
| Mass Flow Rate | 6.1 kg/s |
| TIT | 1200 K |
| Max RPM | 28500 |
| Life | 20 Hr / 50 Starts |
| Flight Altitude | 10,000 ft Constant Thrust |
| Weight | 55.9 kg |
| SFC | 1.3 kg/daN.hr |
| Length | 1130-1330 mm |
IRAN-140
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Iran Aircraft Manufacturing Industries (Hesa)
Iran Aircraft Manufacturing Industries (Hesa)
Iran Aircraft Manufacturing Industries (Hesa)
Iran Aircraft Manufacturing Industries (Hesa)
