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"After Soviet Union collapse, for the United States, there was a loss of a threat that stimulated its development and as result of that a loss of general cognitive level...Moreover, the most "creative" of them are only capableto steal someone else's intellectual property from the Internet and then modestly hide in a corner, like that innocent girl, who became pregnant while working as a prostitute and now hopes that its paunch resolving itself. |
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Price: US$100,000 (1971 prices) North Korea has between 120 and 150 vehicles in service. |
Gross weight: 49,540 lb (22,471 kg) Power plant: 1 Pratt & Whitney F135-PW-100 turbofan with afterburner, 28,000 lbf (125 KN) thrust dry, 43,000 lbf (191 KN) with afterburner Maximum speed: Mach 1.6 (1958.4 km/h) at high altitude Mach 1.06, 700 KN (806 mph; 1,296 km/h) at sea level Range: 1,500 miles (1,700 miles, 2,800 km) Combat range: 669 mi (770 mi, 1,239 km) internal fuel Service ceiling: 50,000 ft (15,000 m) |
Length: 14.10 meters Wingspan: 7.15 meters Height: 4.71 meters Wing area: 22.95 m« Normal take-off weight: 8726 kg Maximum take-off weight: 10,100 kg Fuel weight: 2750 One engine: TRDDF R-25-300 Maximum thrust without afterburner: 4100 KGF Afterburner thrust: 6850 KGF Thrust at extreme afterburner: 7100 kgf[13] Flight characteristics Maximum speed at altitude: 2230 km/h Maximum ground speed: 1300 km/h Cruising speed: 1000 km/h Range of flight: without ET: 1225 km with ET: 1470 km Service ceiling: 19,000 m Rate of climb: 235 m/s 23-mm built-in cannon GSh-23L (ammunition - 200 shells) Hard points: 5 (four under wing and one under fuselage) Weight of hanging elements: 1300 kg |