Data compared between the JAS39C, the JF-17, and the J-10
Length: 14.1m, 14.0m, 16.3m
Wingspan: 8.4m, 8.7m, 9.7m
Height: (excluding landing gear) 3.4m, 3.95m, 4.6m
Empty weight: 5700-6800kg, 6411kg, 9730kg
Max weight: 14000kg, 12700kg, 19277kg
Wing area: 30.2m², 24.4m², 39m²
Internal fuel: 2500kg, 2300kg, 4500kg
Engine thrust dry: 54kN, 49.4kN, 89.17kN
Engine thrust wet: 80.5kN, 84.4kN, 129.4kN
Combat radius: 800km, 1550km with external fuel, 1352km, presumably with external fuel, 2540km, presumably with external fuel
Ferry range: 3500km, 3000km, 3400km
Max speed low alt: M1.2, >M1.0, M1.2
Max speed high alt: M2.0, M1.6-M1.8, M2.2
Climb rate: T/O to 10,000m ~100 sec, T/O to 14,000m in 180sec, N/A, N/A
TWR: 0.97, 0.99, 0.98
Service ceiling: 18,000m, 16,700m, 20,000m
Max G: +9 -3, +8,5 -3, +9 -3
Onset rate: 6-12G/sec, N/A, N/A
Runway length required for operation: 800x9m, N/A, N/A
Take off run: 400m, 500m, <500m
Landing run: 400-500m, 700m, N/A
Turn around time: <10 min, N/A, N/A
MTBF: 7.2h, N/A, N/A
Last edited by Robban on 11 Jun 2009, 14:34, edited 1 time in total.
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