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 |