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Antonov An-26
Military
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Lockheed C-5 Galaxy
Military
|
|
|---|---|---|
| Quick facts | ||
| Manufacturer | Antonov | Lockheed |
| Type | Military transport | Military transport |
| Origin | 🇺🇦 Soviet Union (Ukraine) | 🇺🇸 United States |
| First flight | 1969 | 1968 |
| Status | In service | In service |
| Units built | 1,403 | 131 |
| Unit cost | — | — |
| Dimensions | ||
| Length | 23.80 m | 75.31 m |
| Wingspan | 29.20 m | 67.89 m |
| Height | 8.58 m | 19.84 m |
| Wing area | 75.0 m² | 576.0 m² |
| Weights & fuel | ||
| Empty weight | 15,020 kg | 172,371 kg |
| Max. take-off weight | 24,000 kg | 381,000 kg |
| Max. payload | 5,500 kg | 127,460 kg |
| Performance | ||
| Max. speed | 540 km/h | 919 km/h |
| Cruise speed | 440 km/h | 833 km/h |
| Range | 2,550 km | 4,440 km |
| Service ceiling | 7,500 m | 10,900 m |
| Crew & capacity | ||
| Crew | 5 | 7 |
| Seats (max.) | 40 | — |
| Cargo capacity | 5,500 kg | 127,460 kg |
| Powerplant | ||
| Engines | 2 | 4 |
| Engine type | — | — |
| Engine model | Ivchenko AI-24VT | General Electric F138-GE-100 (C-5M) |
| Thrust (each) | — | 228.0 kN |
| Power (each) | 2,074 kW | — |
At a glance
Figures are compiled from public sources and may be approximate; they can vary by variant and configuration.