Hypothetical size difference between KE-B and KE-C by 2x enlargement, or 40% increase in lenght and width
Length: 20.58m
Span width: 14m
Wing Area: 76m2
Empty Weight: ~8500kg
Wingload at empty weight: 112kg/m2
Endurance: 2.5 times that of similar sized twin engine heavyweight 5th generation supercruise capable fighters. (4x less thrust+20% better fuel consumption but with half the internal fuel load).
View attachment 136207
If Baykar wants to have the Kizilema to have a higher topspeed like other manned fighters in the M1.6-M2.0 range and better sustained turn rate, it could settle for a Kizilelma just 50% larger with 20% increase in length and width, fitted with a 20.000lbf engine weighing ~1060kg (based on AI-9500F weight and comparable engines of the era)
Length: 17.4m
Span width: 12m
Wing Area: 57m2
Empty Weight: ~6300kg
Wingload at empty weight: 111kg/m2
Fuel load: 2280 liters or 1824kg at ambient temperature (2x fuel of KE-B to compensate for 2x increase in thrust)
Max thrust: 20,000lb
TWR at empty weight: 1,44
TWR at full fuel load: 1,12:1
TWR at full fuel load+4 Gökhan/Gökbora at 200kg each: 1,01:1
Actual fuel load might be a bit higher at minimum 2700-2800 liters but for convenience sake I kept it at twice the load compared to KE-B.