Thursday, November 20, 2008

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An-124


Maiden Flight: Friday, December 24, 1982
IOC: 1987
Total Production: 60

An-225 Mriya


IOC: 1988

Also Known As
An-225 Cossack


Origin
Russia


Contractor/s
Antonov ASTC

Family Members
An-124 Ruslan

Power plant:
D-18T (6)

Description: The massive six-engine Antonov An-225 Mriya, NATO referred to by Cossack codename, is the world's largest aircraft produced ever. It was developed to provide highly demanding strategic airlift capability to the Soviet Air Force that couldn't be achieved by the four-engine An-124 Ruslan. Thus, the An-225 aircraft is able to carry payloads larger in size and heavier than the Ruslan. The An-225 is larger than the An-124 tactical transport aircraft. Its airframe evolved from the proven An-124 cargo aircraft despite externally it seems to be a completely distinct aircraft.

It is powered by six engines instead of four and retains the double-deck layout from the An-124 with a more spacious lower deck compartment for wider, large-sized cargo. It is capable of airlifting payloads weighing up to 250 tons, conduct non-stop continental flights carrying between 180 and 200 tons of cargo or intercontinental flights carrying up to 150 tons. In addition, the An-225 can carry single piece payloads of up to 200 tons on the outside of the fuselage such as the Buran space shuttle.

The huge pressurized cargo compartment in the lower deck is 43 meters in length, 6.4 meters width, and 4.4 meters height. The cargo compartment also includes cargo handling system and the front ramp for easy loading/unloading operations. Special cargo can be attached to the fuselage increasing the airlift options for this tactical aircraft. To date, the An-225 has been employed for commercial airlift missions operated by an Ukraine-based agency related to Antonov.

The Antonov company along with Ukraine and Russia are studying the possibility of converting the An-225 into a flying launch platform for future aerospace systems. The flying launch platform will allow to achieve costs reduction of the payloads orbital injections.

Specifications
Accommodation: Crew 6

Dimensions: Height 18.1 m, Length 84 m, Wingspan 88 m

Weights: Payload 250,000 kg (551,146 lb)

Engine/s Performance: Thrust 310,320 lb (140,761 kg)

Performance: Ceiling 12,000 m (39,370 ft), Max Range 14,000 km (7,559 nm), Min Range 4,000 km (2,160 nm), Top Speed 237 mps (Mach 0.71)

Other: Number of Engines 6

Operators

Ukraine



Image Gallery


Notes
(*) lead contractor
IOC: Initial Operating Capability
FOC: Full Operating Capability
CEP: Circular Error Probable
Comm: Commissioning Date
Meters (m)   Kilometers (km)   Nautic Miles (nm)   Inch (in)   Yard (yd)   Foot (ft)   Millimeter (mm)
Pound (lb)   Kilogram (kg)   kN (KiloNewton)   Ton (t)
Meters per Second (mps)   Kilometers per Hour (kph)   Knot (kt)   Miles per Hour (mph)
Liter (l)   Galon (gl)
Year (yr)   Minutes (min)   Second (sec)
Shaft-Horse-Power (shp)


Last Updated: Saturday, October 25, 2008

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