| Technical data | ||
|---|---|---|
| Type | MiG-17 | MiG-17F |
| Function | fighter | |
| Year (test/service) |
1950/ 52 | 1951/ 53 |
| Crew | 1 | |
| Engines | 1*VK-1 | 1*3380kg VK-1F |
| Wing Span | 9.63m | |
| Length | 11.26m | |
| Height | 3.80m | |
| Wing Area | 22.60m2 | |
| Weight | Empty 3798kg Loaded 5202kg |
Empty 3930kg loaded 5340kg Maximum 6075kg |
| Speed | 1114km/h | 1145km/h |
| Climb | 45m/sec | 65m/sec |
| Ceiling | ? | 15100m |
| Range | 2150km (external tanks) |
1470km (external tanks) |
| Armament | 1*g37mm 2*g23mm |
1*g37mm 2*g23mm bombs/rockets(u.g.) 500kg |
This was a thoroughly redesigned MiG-15. Original MiG-17 had same engine (VK-1) as a MiG-15 series, but most produced MiG-17F had an improved afterburning VK-1F as wall as variable nozzle.
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 USAF 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 Despite outdated, it was preferred by some Vietnamese aces (Col.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).
| Modified December 5, 1996 |
|
Back to Main Gate |