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MIG-17 | ||
Front-line fighter | ||
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Specifications: | |
Year deployed Wing span, m Lenght, m Height, m Wing area, m2 Weight empty, kg Fuel, kg Take-off Weight, kg: - normal - Maximum Maximum landing weight, kg Engines - in MIG-17F Maximum Thrust, kN(kgs): - VK-1A - VK-1F (afterb./dry.) Maximum speed, km/h: - on sea level - in altitude 3000 m - in altitude 10000 m Service ceiling, m: - dry - afterburner Range, m: - in altitude - with 2 AFT Maximum overload Crew Armament: |
- 1951 - 9,63 - 11,26 - 3,80 - 22,60 - 5340 - 1170 - 5340 - 6070. - 4165 - TJE VK-1A - TJE VK-1F - 26,5 (2700 ), - 33,1/25,5 (3380/2600). - 1100, - 1145, - 1071. - 16600, - 15100. - 1240 - 940 - 8. - 1 MIG-17 - 1 cannon N-37D (40 rounds) 2 cannons NR-23 (2У80 rounds). In 2 hardpoints: bombs 100 or 50 kg or AFT 400 l. MIG-17F - 1 cannon N-37D (40 rounds) 2 cannons NR-23 (2У80 rounds). 4 UR TTU-190 or 2 ATU-212 (212 mm); or 2 bombs 50, 100 or 250 kg. MIG-17P - 3 cannons NR-23 with 100 rounds N MIG-17PFU - 4 AAM K-5 (RS-2US) MIG-17R - 2 cannons NR-23 with 100 rounds |