Antonov An-22 | |
|---|---|
| Land | Sovjetunionen |
| Typ | Strategisk luftlyftare |
| Första flygningen | 27 februari 1965 |
| Byggd | 69 |
Den Antonov An-22 "Antei" (ryska: Ан-22 Антей, An-22 Antej; Antaeus) (NATO-rapporteringsnamn "Cock") är ett tungt militärt transportflygplan konstruerat av Antonov Design Bureau i Sovjetunionen. Drivs av fyra turbopropmotorer som var och en driver ett par motroterande propellrar, designen var det första bredkroppade transportflygplanet och är fortfarande världens största turbopropdrivna flygplan hittills. An-22 dök först upp offentligt utanför Sovjetunionen vid Paris Air Show 1965. Därefter såg modellen omfattande användning i stora militära och humanitära luftbroar för Sovjetunionen och är fortfarande i tjänst med det ryska flygvapnet.
Källkod: Antonov An-22 på Wiki
| Antonov An-22 Gå runt | |
|---|---|
| Fotograf | Unknow |
| Lokalisering | Unknow |
| Bilder | 24 |
General Characteristics
The Antonov An-22 Antei (Antaeus) was the world’s first wide-body aircraft and, for a time, the largest aircraft in the world until the introduction of the Lockheed C-5 Galaxy. Designed by the Antonov Design Bureau in the 1960s, it was the Soviet Union’s primary heavy strategic airlifter, capable of transporting main battle tanks, missile launchers, and oversized military equipment. The aircraft is distinguished as the largest turboprop-powered aircraft ever built, featuring massive contra-rotating propellers for exceptional short-field performance and the ability to operate from unpaved airstrips.
| Property | Typical Value |
|---|---|
| Roll | Heavy Strategic Transport/Airlifter |
| National Origin | Sovjetunionen |
| First Flight | February 27, 1965 |
| No. Built | ~67–70 (Total production) |
| besättning | 5–6 (Pilot, Co-pilot, Navigator, Flight Engineer, Radio Operator) |
| längd | 57.92 m (190 ft 0 in) |
| Spännvidd | 64.40 m (211 ft 3 in) |
| Max Takeoff Weight | 250,000 kg (551,156 lb) |
Cargo and Capabilities
- Maximum Payload: 80,000 kg (176,370 lb).
- Cargo Hold Dimensions (L x W x H): Approx. 33 m x 4.4 m x 4.4 m (108 ft 3 in x 14 ft 5 in x 14 ft 5 in).
- Cargo Hold Volume: Approximately 639 m³.
- Loading System: Features a rear loading ramp and integral cargo handling systems (winches, telphers).
- Cargo Compartment: The main cargo hold is unpressurized, allowing the rear doors to be opened in flight for paratroop or equipment drops.
- Passenger/Troop Capacity: Forward cabin is pressurized for up to 28 passengers/troop attendants, or up to 292 soldiers in the cargo hold.
Powerplant and Performance
- Engine: 4 x Kuznetsov NK-12MA turboprop engines.
- Power Output (each): 11,000 kW (15,000 shp equivalent).
- Propellers: 8-bladed contra-rotating constant-speed reversible-pitch propellers (4 blades per hub).
- Maximum Speed: 740 km/h (460 mph).
- Cruise Speed: 600–680 km/h (375–423 mph).
- Range (Max Payload): 5,000 km (3,100 mi).
- Ferry Range (Max Fuel): 10,950 km (6,800 mi).
- Short Field Capability: Achieved by powerful engines and large double-slotted flaps, creating a significant slipstream effect over the wing.
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