| PERFORMANCE | WEIGHT | ||
| Maximum speed at sea level | 550 kias | Empty | 12,750 lbs. |
| Max speed at altitude: | .091 mi. | Max vertical takeoff weight | 19,500 lbs. |
| Combat radius | 300 nmiles | Max STO weight: | 32,000 lbs. |
| PROPULSION | Max ordnance load: | 9,200 lbs. | |
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Power Plant: Rolls-Royce Pegasus II (F402) with a thrust of 22,000 lbs. |
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