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Lockheed Martin C-130J Super Hercules
Military
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Lockheed C-130H Hercules
Military
|
|
|---|---|---|
| Quick facts | ||
| Manufacturer | Lockheed Martin | Lockheed |
| Type | Military transport | Military transport |
| Origin | 🇺🇸 United States | 🇺🇸 United States |
| First flight | 1996 | 1954 |
| Status | In production | In service |
| Units built | — | — |
| Unit cost | — | — |
| Dimensions | ||
| Length | 29.79 m | 29.79 m |
| Wingspan | 40.41 m | 40.41 m |
| Height | 11.84 m | 11.84 m |
| Wing area | 162.1 m² | 162.1 m² |
| Weights & fuel | ||
| Empty weight | 34,274 kg | 34,382 kg |
| Max. take-off weight | 79,380 kg | 70,307 kg |
| Max. payload | 19,090 kg | 19,090 kg |
| Performance | ||
| Max. speed | 671 km/h | 592 km/h |
| Cruise speed | 643 km/h | 540 km/h |
| Range | 3,334 km | 3,800 km |
| Service ceiling | 8,615 m | 10,060 m |
| Crew & capacity | ||
| Crew | 3 | 5 |
| Seats (typical) | 92 | — |
| Seats (max.) | 128 | 92 |
| Cargo capacity | — | 19,090 kg |
| Powerplant | ||
| Engines | 4 | 4 |
| Engine type | — | — |
| Engine model | Rolls-Royce AE 2100D3 | Allison T56-A-15 |
| Power (each) | 3,458 kW | 3,424 kW |
At a glance
Figures are compiled from public sources and may be approximate; they can vary by variant and configuration.