Origin: | Mikoyan Design Bureau | ||
Type: | Light Weight Air Superiority Fighter | ||
Crew: | Pilot | ||
First Flight: | 1952 | ||
Engine(s): | 1x VK-1F Turbojet (late versions Have Afterburner) | ||
Thrust: | 3 406 kg (7,495 lbs) | ||
Max. Speed: | 1 137 kph (711 mph) | ||
Cruising Speed: | unknown | ||
Range: | 2 240 Km (1,400 miles) | ||
Ceilling: | 16 769 m (54,500 ft) | ||
Rate of Climb: | unknown | ||
Height: | 3.3 m (11 ft) | ||
Length: | 11 m (35.75 ft) | ||
Width: | 9.6 m (31.2 ft) | ||
Weight(loaded): | 6 081.36 kg (13,379 lbs) | ||
Cannon: | 3x 23mm Cannons | ||
Air-Air: | Late Variants have Alkali Radar Homing Missiles | ||
Air-Surface: | Unguided Bombs, Rockets |