Engine |
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Engine name | Number | Basic mass | Wing loading |
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Klimov RD-33 | 2 | 11,130 kg | 384 kg/m2 |
Payload weight:
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Engine characteristics | Mass with fuel |
Max Gross Weight |
||||
Weight (each) | Type | 30% (8m) |
100% (29m)
|
134% (29+10m) | ||
1,050 kg | Afterburning low-bypass turbofan | 12,166 kg | 14,583 kg | 15,757 kg | 17,738 kg | |
Maximum engine thrust @ 0 m (RB/SB) | Thrust to weight ratio @ 0 m (WEP) | |||||
Condition | 100% | WEP | ||||
Stationary | 3,920 kgf | 6,816 kgf | 1.12 | 0.93 | 0.87 | 0.77 |
Optimal | 5,430 kgf (1,575 km/h) |
12,445 kgf (1,575 km/h) |
2.05 | 1.71 | 1.58 | 1.40 |
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