| Technical data | |
|---|---|
| Type | MiG-17 |
| Function | fighter |
| Year (test/service) |
1950/52 |
| Crew | 1 |
| Engines | 1*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 |
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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.
Original MiG-17 had modified (but not afterburning) engine VK-1A.
Production was also undertaken in Poland (LIM-5), China (Jian-5) and Czechoslovakia. The aircraft is used by at least 25 countries (Soviet-built or Chinese J-5 fighters, JT-5 trainers).
During Vietnam war MiG-17 were used by North Vietnam AF against UASF aircraft. Despite outdated, it was preferred by some Vietnamese aces (Col. Tomb) for its agility and powerful cannons. Indeed it was MiG-17's guns that turned down 'missile only' fighters development in both USSR and USA (see a letter from Dave Sutton, private MiG owner).
Now is one of hot items in collections of private pilots.
| Prototype | Series variants | Experimental | |||
|---|---|---|---|---|---|
| I-330/SI | MiG-17P - limited all-weather version with the Izumrud fixed-scan radar and 37mm cannon replaced with third 23mm one. VK-1 engine. |
MiG-17F |
I-340/SM-1 |
I-350 (M-1, M-2, MT) |
I-360/SM-2 |
|
MiG-17PF |
MiG-17PFU - all-weather version with deleted guns and four K-5 (ARS-212) beam-riding underwing missiles. 1953 | SP-2 | SR-2 |
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| Modified December 5, 1996 |
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