F-84 Thunderjet vs J-11 Responsive Dragon
Overview
The F-84 Thunderjet and the J-11 Responsive Dragon are both Combat Aircraft, manufactured by Republic and Shenyang respectively.
The J-11 Responsive Dragon reaches 2,500 km/h β 2.5x the F-84 Thunderjet's 1,001 km/h. The F-84 Thunderjet has an operational range of 1,080 km vs 3,530 km for the J-11 Responsive Dragon. The J-11 Responsive Dragon operates at altitudes up to 18,500 m compared to 12,344 m for the F-84 Thunderjet. At 33,000 kg MTOW, the J-11 Responsive Dragon is 3.1x the F-84 Thunderjet's 10,590 kg.
The F-84 Thunderjet has been produced in 7,524 units vs 442 for the J-11 Responsive Dragon. Unit cost is $1.4M for the F-84 Thunderjet vs $30M for the J-11 Responsive Dragon. The F-84 Thunderjet first flew 52 years before the J-11 Responsive Dragon (1946 vs 1998).
| American fighter-bomber of the 1940sβ1950s era, notable in the Korean War for close air support and strategic bombing missions. | |
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| Origin country | πΊπΈ United States |
| Category | Combat Aircraft |
| Manufacturer | Republic |
| First flight | 28 February 1946 |
| Year introduced | 1950 |
| Number produced | 7524 units |
| Average unit price | $1.4 million |
| Chinese modernized variant of the Soviet Su-27 Flanker twin-engine combat aircraft. | |
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| Origin country | π¨π³ China |
| Category | Combat Aircraft |
| Manufacturer | Shenyang |
| First flight | 1 January 1998 |
| Year introduced | 1998 |
| Number produced | 442 units |
| Average unit price | $30 million |
| Wing area | 24.0 mΒ² β |
| Wingspan | 11.1 m β |
| Height | 3.8 m β |
| Length | 11.6 m β |
| Maximum speed | 1001 km/h β |
| Operational range | 1,080 km β |
| Service ceiling | 12,344 m β |
| Max. takeoff weight | 10,590 kg β |
| Empty weight | 5,200 kg β |
| Total thrust | 1 x 2,522 kgf β |
| Wing area | 52.8 mΒ² β |
| Wingspan | 14.7 m β |
| Height | 5.9 m β |
| Length | 21.9 m β |
| Maximum speed | 2500 km/h β |
| Operational range | 3,530 km β |
| Service ceiling | 18,500 m β |
| Max. takeoff weight | 33,000 kg β |
| Empty weight | 16,380 kg β |
| Total thrust | 2 x 7,650 kgf β |
Performance Radar Chart
Detailed Comparison
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