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BAE Harrier II Specifications
BAE Harrier II
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| Data for Aircraft | BAE Harrier II |
| Year Introduced | 1989 |
| Number Built | 143 |
| Rotor Diameter | |
| Wingspan | 30 ft 4 in (9.25 m) |
| Aspect Ratio | |
| Disc Loading | |
| Height | 11 ft 8 in (3.56 m) |
| Wing Area | 343 ft² (22.6 m²) |
| Wing Loading | |
| Length | 46 ft 4 in (14.12 m) |
| Lift-to-Drag Ratio | |
| Engine Type | Rolls-Royce Pegasus Mk. 105, 21,750 lb (96.7 kN) |
| Country of Origin | Britain |
| Empty Weight | 12,500 lb (5,700 kg) |
| Max Landing Weight | |
| Max Ramp Weight | 18,950 lb VTO, 31,000 lb STO (8,595 kg VTO, 14,061 kg STO) |
| Useful Load | 18,500 lb |
| Seats | 1 |
| Crew | 1 |
| Power Loading | |
| Thrust to Weight | |
| Cockpit Length | |
| Cockpit Width | |
| Cockpit Height | |
| Load Limit Negative | |
| Load Limit Positive | |
| Fuel Capacity | |
| Oil Capacity |
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