Antonov An-225 Mriya

Antonov An-225 Mriya

ZemljaSovjetski Savez
TipNadmašite teretne teretne avione
Prvi let21 decembar 1988
Izgradio1

Čaj Antonov An-225 Mriya (на језику: најбољи Бе-225 Мрія, lit. 'dream' or 'inspiration'; Ime za izveštavanje NATO-a: Kozak) je strateški teretni avion koji je projektovao Biro za dizajn Antonova u ukrajinskom SSR-u unutar Sovjetskog Saveza tokom osamdesetih godina. Napaja ga šest turbofan motora i najteži je avion ikada napravljen, sa maksimalnom težinom poletanja od 640 tona (710 kratkih tona; 630 dugih tona). Takođe ima najveći raspon krila od svih aviona u operativnoj službi.

Izvor: Antonov An-225 Mriya on Wiki

Antonov An-225 Mriya Walk Around
FotografVladimir Gunkalo
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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
Ulogu Strategic Airlift Cargo, Space Shuttle Carrier
National Origin Soviet Union / Ukraine
First Flight December 21, 1988
No. Built 1 (Completed and operational)
Posada 6–7 (Flight crew)
Dužina 84.0 m (275 ft 7 in)
Raspon krila 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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