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Developing Nation: |
USSR. |
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Task: |
Multirole fighter. |
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First Flight: |
April 20, 1981. |
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Crew: |
1 or 2 in tandem. |
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Wing Span: |
14,70 m. |
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Wing Area: |
62,04 mē. |
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Length: |
21,94 m. |
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Engine (s): |
Saturn Lyalka AL-31F
Turbofan. Thrust without afterburners: 79,4 kN.
Thrust with afterburners
122,59 kN (2x). |
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Weight: |
16.380 kg. |
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Max.Take off weight: |
28.300 kg. |
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Fuel and load: |
- Internal fuel tanks,
normally 5.270 kg. maximum 9.400 kg. or 12.000 liters in 3
fuselage tanks.
- Theoretical weapons load:
Normally 4.000 kg.
Maximum 8.000 kg. |
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Max. Speed: |
- at sea-level 1.370 km/h.
- at cruising altitude 2.280
km/h. |
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ceiling: |
18.500 m. |
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Max. Range: |
- at cruising altitude 3.680
km.
- at sea level 1.370 km. |
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Weapons: |
- fixed Gsh-30 30 mm cannon.
- Air to air missiles Vympel
R-73 and Vympel R-27. |
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Posters
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