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