|
This was a thoroughly redesigned MiG-15. Changes
included absolutely new thin wing, a lengthened rear fuselage, increased tail surfaces, wider-track landing gear and ventral
fin (added after prototype tests). Also revised were airbrakes and cockpit instrumentation.
| Technical data | |||||||
|---|---|---|---|---|---|---|---|---|
| Type | MiG-17 | |||||||
| Function | fighter | |||||||
| Year (test/service) |
1950/52 | |||||||
| Crew | 1 | |||||||
| Engines | 1*Klimov VK-1A | |||||||
| Wingspan | 9.63m | |||||||
| Length | 11.26m | |||||||
| Height | 3.80m | |||||||
| Wing Area | 22.60m2 | |||||||
| Empty Weight | 3798kg | |||||||
| Weight Loaded | 5202kg | |||||||
| Speed | 1114km/h | |||||||
| Climb | 45m/sec | |||||||
| Ceiling | ? | |||||||
| Range | 2150km (external tanks) | |||||||
| Armament | 1*g37mm
2*g23mm | |||||||
| ||||||||
| Modified December 5, 1996
by Alexandre Savine; |
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