موتوری مانند اردی 33 برای هر جنگنده متوسط دو عدد نیاز است
در مورد اردی 93 یک الی دو
و ال 31 یک موتور کافی است
ترکیه پیش از این با موتور هایF110و F100سروکار داشته

RD33&93

Performance

Maximum thrust: 50.0 kN (11,230 lbf) dry, 81.3 kN (18,285 lbf) afterburning.

Overall pressure ratio: 21:1

Bypass ratio: 0.49

Air mass flow: 75.5 kg/s (166.5 lbm/s)

Turbine inlet temperature: 1,407 °C (2,565 °F)

Specific fuel consumption: 75 kg/(kN·h) (0.77 lb/(lbf·h)) dry, 188 kg/(kN·h) (1.85 lb/(lbf·h))

Thrust-to-weight ratio: 4.82 (dry), 7.9 (afterburning)

Life expectancy: 4,000 hours

The Klimov poster at Zhuhai 2010 airshow gave the thrust range of the engine to be 49.4 kN to 84.4 kN Wet.

F100

Performance

Maximum thrust:

14,590 pounds-force (64.9 kN) military thrust,

23,770 pounds-force (105.7 kN) with afterburner

Overall pressure ratio: 25:1

Specific fuel consumption: Military thrust: (0.73 lb/(lbf·h))

Thrust-to-weight ratio: 7.4:1

@irospace

F110

Performance
Maximum thrust:
Military power: 17,155 lbf (76.31 kN)
Full afterburner: 29,400 lbf (131 kN)
Overall pressure ratio: 30.7:1
Air mass flow: 270 lb/s (122.4 kg/s)
Turbine inlet temperature: 2,750 °F (1,510 °C)[16]
Thrust-to-weight ratio: 4.38:1 military power, 7.50:1 in afterburner

Al 31

Performance
Maximum thrust:
74.6 kN (16,800 lbf) dry thrust
122.6 kN (27,600 lbf) with afterburner
Overall pressure ratio: 23:1
Bypass ratio: 0.56:1
Air mass flow: 112 kg/s (250 lb/s)
Turbine inlet temperature: 1,665 K (2,537 °F; 1,392 °C)
Specific fuel consumption:
Dry thrust: 22.1 g/kN/s (0.78 lb/lbf/h)
With afterburner: 55.5 g/kN/s (1.96 lb/lbf/h)
Thrust-to-weight ratio: 4.93 (dry), 8.22 (afterburning)

@irospace