
Antonov An-225 Mriya | |
|---|---|
| País | Unión Soviética |
| Tipo | Aviones de carga de gran tamaño |
| Primer vuelo | 21 de diciembre de 1988 |
| Construido | 1 |
el Antonov An-225 Mriya (Ucraniano: Антонов Ан-225 Мрія, lit. 'sueño' o 'inspiración'; Designación OTAN: Cosaco) es un avión estratégico de carga de transporte aéreo que fue diseñado por la Oficina de Diseño Antonov en la RSS de Ucrania dentro de la Unión Soviética durante la década de 1980. Está propulsado por seis motores turbofán y es el avión más pesado jamás construido, con un peso máximo de despegue de 640 toneladas (710 toneladas cortas; 630 toneladas largas). También tiene la mayor envergadura de cualquier avión en servicio operativo.
Fuente: Antonov An-225 Mriya en Wiki
| Antonov An-225 Mriya caminar alrededor | |
|---|---|
| Fotógrafo | Vladimir Gunkalo |
| Localización | Unknow |
| Fotos | 26 |
Ver también:
General Characteristics
The Antonov An-225 Mriya (meaning “Dream” in Ukrainian) was the largest and heaviest aircraft ever built. Developed by the Antonov Design Bureau in the Soviet Union (Ukrainian SSR) during the 1980s, it was originally designed to transport the **Buran-class space shuttle** and components of the Energia rocket on its external fuselage. After the Soviet space program ended, the sole completed aircraft was refurbished and operated commercially by Antonov Airlines, specializing in transporting ultra-heavy and oversized cargo globally. The aircraft was tragically destroyed in February 2022.
| Property | Typical Value |
|---|---|
| Papel | Strategic Airlift Cargo, Space Shuttle Carrier |
| National Origin | Soviet Union / Ukraine |
| First Flight | December 21, 1988 |
| No. Built | 1 (Completed and operational) |
| Equipo | 6–7 (Flight crew) |
| Longitud | 84.0 m (275 ft 7 in) |
| Envergadura | 88.4 m (290 ft 0 in) |
| Max Takeoff Weight | 640,000 kg (1,411,000 lb / 640 tonnes) |
Cargo and Payload
- Maximum Internal Payload: **250,000 kg (250 tonnes)**.
- Maximum External Payload (Buran shuttle): 200,000 kg (200 tonnes).
- Cargo Hold Dimensions (L x W x H): 43.5 m x 6.4 m x 4.4 m (142 ft 8 in x 21 ft 0 in x 14 ft 5 in).
- Cargo Hold Volume: Approximately 1,300 m³.
- Loading System: Features a hinged nose section that opens upward and a built-in overhead crane system. There is no rear cargo ramp (unlike the An-124).
- Landing Gear: **32 wheels** (20 of which were steerable) to distribute its immense weight.
Powerplant and Performance
- Engine: 6 x ZMKB Progress Lotarev D-18T turbofan engines.
- Thrust (each): ~229.5 kN (~51,600 lbf).
- Total Thrust: Over 1,377 kN (309,600 lbf).
- Maximum Speed: 850 km/h (530 mph).
- Cruise Speed: 800 km/h (500 mph).
- Range (Maximum Fuel): 15,400 km (9,600 mi).
- Range (With 200-tonne payload): 4,000 km (2,500 mi).
- Service Ceiling: 11,000 m (36,100 ft).
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