Engine |
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Engine name | Number | Basic mass | Wing loading |
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General Electric J85-GE-21A | 2 | 4,945 kg | 402 kg/m2 |
Payload weight:
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Engine characteristics | Mass with fuel |
Max Gross Weight |
||||
Weight (each) | Type | 30% (11m) |
100% (38m)
|
169% (38+26m) | ||
303 kg | Afterburning axial-flow turbojet | 5,544 kg | 6,940 kg | 8,317 kg | 9,946 kg | |
Maximum engine thrust @ 0 m (RB/SB) | Thrust to weight ratio @ 0 m (WEP) | |||||
Condition | 100% | WEP | ||||
Stationary | 1,480 kgf | 2,220 kgf | 0.80 | 0.64 | 0.53 | 0.45 |
Optimal | 1,575 kgf (1,458 km/h) |
3,011 kgf (1,458 km/h) |
1.09 | 0.87 | 0.72 | 0.61 |
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