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Lockheed Martin C-130J Super Hercules
Military
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Boeing C-17 Globemaster III
Military
|
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|---|---|---|
| Quick facts | ||
| Manufacturer | Lockheed Martin | Boeing |
| Type | Military transport | Military transport |
| Origin | 🇺🇸 United States | 🇺🇸 United States |
| First flight | 1996 | 1991 |
| Status | In production | In service |
| Units built | — | 279 |
| Unit cost | — | US$ 218 million |
| Dimensions | ||
| Length | 29.79 m | 53.04 m |
| Wingspan | 40.41 m | 51.75 m |
| Height | 11.84 m | 16.79 m |
| Wing area | 162.1 m² | 353.0 m² |
| Weights & fuel | ||
| Empty weight | 34,274 kg | 128,100 kg |
| Max. take-off weight | 79,380 kg | 265,350 kg |
| Max. payload | 19,090 kg | 77,519 kg |
| Performance | ||
| Max. speed | 671 km/h | — |
| Cruise speed | 643 km/h | 830 km/h |
| Max. Mach | — | Mach 0.76 |
| Range | 3,334 km | 4,480 km |
| Ferry range | — | 10,390 km |
| Service ceiling | 8,615 m | 13,716 m |
| Crew & capacity | ||
| Crew | 3 | 3 |
| Seats (typical) | 92 | 102 |
| Seats (max.) | 128 | 134 |
| Powerplant | ||
| Engines | 4 | 4 |
| Engine type | — | — |
| Engine model | Rolls-Royce AE 2100D3 | Pratt & Whitney F117-PW-100 |
| Thrust (each) | — | 180.0 kN |
| Power (each) | 3,458 kW | — |
At a glance
Figures are compiled from public sources and may be approximate; they can vary by variant and configuration.