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Hawker Siddeley Nimrod Specifications
Hawker Siddeley Nimrod
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| Data for Aircraft | Hawker Siddeley Nimrod |
| Year Introduced | 1969 |
| Number Built | 49 |
| Rotor Diameter | |
| Wingspan | 35.00 m (114 ft 10 in) |
| Aspect Ratio | |
| Disc Loading | |
| Height | 9.14 m (31 ft) |
| Wing Area | 197.05 m² (2,121 sq ft) |
| Wing Loading | |
| Length | 38.65 m (126 ft 9 in) |
| Lift-to-Drag Ratio | |
| Engine Type | Rolls-Royce Spey, 54.09 kN (12,160 lbf) |
| Country of Origin | Britain |
| Empty Weight | 39,009 kg (86,000 lb) |
| Max Landing Weight | |
| Max Ramp Weight | 87,090 kg (192,000 lb) |
| Useful Load | 106,000 lb |
| Seats | 24 |
| Crew | 12 |
| 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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