
アントノフ An-225 ムリヤ | |
|---|---|
| 国 | ソ連 |
| 型 | アウトサイズ貨物貨物機 |
| 初飛行 | 1988年12月21日 |
| 構築 | 1 |
ザ アントノフ An-225 ムリヤ (ウクライナ語:225「夢」または「インスピレーション」を点灯。NATO報告名:コサック)は、1980年代にソ連内のウクライナSSRのアントノフ設計局によって設計された戦略的空輸貨物機です。それは6つのターボファンエンジンによって動力を与えられ、640トン(710短いトン;630の長いトンの)の最高離陸重量で、今まで建てられた最も重い航空機である。また、運用サービスで任意の航空機の最大の翼幅を持っています。
ソース: アントノフ An-225 ウィキのムリヤ
| アントノフ AN-225 ムリヤ・ウォーク・アラウンド | |
|---|---|
| カメラマン | ウラジーミル・グンカロ |
| ローカライズ | 知りません |
| 写真 | 26 |
関連項目:
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 |
|---|---|
| 役割 | Strategic Airlift Cargo, Space Shuttle Carrier |
| National Origin | Soviet Union / Ukraine |
| First Flight | December 21, 1988 |
| No. Built | 1 (Completed and operational) |
| 乗組員 | 6–7 (Flight crew) |
| 長さ | 84.0 m (275 ft 7 in) |
| 翼 | 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).
再生 : 1102


















