JF-17 Thunder Specification
General |
Crew |
One |
Maiden Flight |
August, 2003 |
Type |
Multi-Role |
Cost |
$15m-$25m |
Dimensions |
Length |
14.9 m |
49 ft |
Height |
4.77 m |
15.6 ft |
Wing Area |
24.4 m² |
263 ft² |
Weights |
Empty Weight |
6,411 kg |
14,134 lb |
Maximum Take-Off Weight |
12,474 kg |
27,500 lb |
Maximum Landing Weight |
7,802 kg |
17,200 lb |
Fuel Weight |
2,268 kg |
5000 lb |
Performance |
Maximum Speed |
1,910 km/h – 1,187 m/h |
1.6 Mach |
Ferry Range |
2,037 km |
1,266 miles |
Operational Radius |
1,352 km |
850 miles |
Service Ceiling |
16,794 m |
55,500 ft |
Thrust/Weight |
0.95 |
|
G-Limit |
+8 / -3 |
|
Hardpoints |
7 |
|
Engine |
Name |
Klimov RD-93 |
Guizhou WS-13 |
Type |
Turbofan |
Turbofan |
Origin |
Russia |
China |
Number of Engines |
One |
One |
Dry Thrust |
49.4 kN |
51.2 kN |
Thrust After Burner |
84.4 kN |
86.37 kN | | | |
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