Apologies if this has been posted before since I have been away for some time. If that is the case, simply delete this thread.
Check it out at
Pakistan Aeronautical Complex
Notice the updated information about JF-17 Thunder, particularly the thrust-to-weight ratio which is stated to be around 1.01.
Physical
Length 47 ft
Height 15.5 ft
Wingspan 31 ft
Empty Weight 14,520 lb
Performance
Maximum Take Off Weight 27,300 lb
Max Mach No 1.6
Maximum Speed 700 Knots IAS
Service Ceiling 55,500 ft
Thrust to Weight Ratio 1.01 approx
Maximum Engine Thrust 19,180 lb
G Limit +8,-3
Ferry Range 1,880 NM
Armament
No of Stations 07
Total Load Capacity 8000 lb
NBunless this is a mistake) note it states that PAC will have exclusive rights to manufacture 58% of the airframe.
The Pakistan Aeronautical Complex (PAC) Kamra has updated its website.
Check it out at
Pakistan Aeronautical Complex
Notice the updated information about JF-17 Thunder, particularly the thrust-to-weight ratio which is stated to be around 1.01.
Physical
Length 47 ft
Height 15.5 ft
Wingspan 31 ft
Empty Weight 14,520 lb
Performance
Maximum Take Off Weight 27,300 lb
Max Mach No 1.6
Maximum Speed 700 Knots IAS
Service Ceiling 55,500 ft
Thrust to Weight Ratio 1.01 approx
Maximum Engine Thrust 19,180 lb
G Limit +8,-3
Ferry Range 1,880 NM
Armament
No of Stations 07
Total Load Capacity 8000 lb
NBunless this is a mistake) note it states that PAC will have exclusive rights to manufacture 58% of the airframe.