Antonov An-22 – Fotos e Vídeos

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Antonov 22 Um Galo

Antonov An-22

PaísUnião Soviética
TipoAirlifter estratégico
Primeiro voo27 de fevereiro de 1965
Construído69

O Antonov An-22 "Antei" (Russo: Ан-22 Антей, An-22 Antej; Antaeus (nome de reportagem da OTAN "Cock") é um avião de transporte militar pesado projetado pelo Antonov Design Bureau na União Soviética. Alimentado por quatro motores turboélices cada um dirigindo um par de hélices contra-rotativas, o design foi a primeira aeronave de transporte de corpo largo e continua sendo a maior aeronave turboélice do mundo até o momento. O An-22 apareceu publicamente fora da União Soviética no Paris Air Show de 1965. Depois disso, o modelo viu uso extensivo em grandes transportes aéreos militares e humanitários para a União Soviética, e ainda está em serviço com a Força Aérea Russa.

Fonte: Antonov An-22 na Wiki

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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
Papel Heavy Strategic Transport/Airlifter
National Origin União Soviética
First Flight February 27, 1965
No. Built ~67–70 (Total production)
tripulação 5–6 (Pilot, Co-pilot, Navigator, Flight Engineer, Radio Operator)
comprimento 57.92 m (190 ft 0 in)
Envergadura 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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