Antonov An-225 Mriya Specs, Engines, Weight, Cockpit, and Price – The Antonov An-225 Mriya is a strategic six-engine heavy transport aircraft and designed and manufactured by the Antonov Design Bureau (ADB) of Ukraine. The term Mriya refers to dream words or inspiration in English. The name NATO reporting is Cossack.
The Antonov Design Bureau (ADB) developed two An-225 Mriya prototypes. The first prototype development began in early 1984 and the inaugural flight took place in December 1988. It began operations in 1989.
Modifications include lengthening the fuselage and wingspan, adding two engines, redesigning the tail with twin vertical fins, increasing the number of landing gear tires to 32 and removing rear cargo doors. The aircraft initially had a maximum gross weight of 600t which increased to 640t with additional floor area under the $ 20 million increase program.
The development of the second prototype began in the late 1980s with the aim of achieving a more effective cargo transport aircraft. The prototype is enhanced with a redesigned rear cargo and tail door that is equipped with a vertical stabilizer.
Loads that are too large can be carried on a wide cargo deck and on an externally mounted mount. Cossack has an air cargo handling system and cargo door equipped with slopes to carry out loading and unloading missions quickly and easily. It is also equipped with airplane barrel extensions on the front and rear wings to increase range. Load security system installs uniquely sized payloads to the upper fuselage parts.
The aircraft is equipped with a 32 wheel landing gear system. The landing nose features four wheels on the front of the fuselage. The rear body consists of 16 wheels that can be reduced from 28 tires mounted on the main landing gear. This aircraft can turn full on a runway as wide as 60m.
It is equipped with bucket-shaped push-in, jetpipe, drive box, exhaust nozzle, fan turbine, combustion chamber, intermediate drive, fan stator blades and fan wheels. The length and width of the machines are 5.4 m and 2.7 m respectively. He is 2.9 m tall. The dry weight is 4,100kg. Service life is 24,000 hours.
The An-225 Mriya can fly with a maximum speed of 850 km / hour. The cruising speed is 800 km / hour. The range of aircraft varies between 4,000 km and 15,400 km.
This aircraft can reach non-stop intercontinental flights while accommodating 180t or 200t payload. It also can carry out intercontinental air transportation with a weight of 150 tons. It can carry 16 standard UAC-10 aeronautical containers, each weighing 10t, 50 cars, turbines, generators, dump trucks, Belaz, Kamatsu and Euclid.
The Antonov Design Bureau (ADB) developed two An-225 Mriya prototypes. The first prototype development began in early 1984 and the inaugural flight took place in December 1988. It began operations in 1989.
Modifications include lengthening the fuselage and wingspan, adding two engines, redesigning the tail with twin vertical fins, increasing the number of landing gear tires to 32 and removing rear cargo doors. The aircraft initially had a maximum gross weight of 600t which increased to 640t with additional floor area under the $ 20 million increase program.
The development of the second prototype began in the late 1980s with the aim of achieving a more effective cargo transport aircraft. The prototype is enhanced with a redesigned rear cargo and tail door that is equipped with a vertical stabilizer.
Antonov An-225 Mriya Variant
The Antonov An-225 Mriya has three variants: An-224, An-225-100 and An-325. An-224 is the original designation of An-225. This variant has an additional rear cargo door. An-225-100 is an improved version of the An-225. This variant is enhanced by better communication equipment, navigation equipment, and traffic collision avoidance systems (TCAS) for use in commercial operations. An-325 is an extended variant of the An-225. It is equipped with an additional engine on each board on board, which increases cargo carrying capacity.Antonov An-225 Mriya Specs
The Antonov An-225 Mriya is designed to carry out military and civilian operations even in the worst weather conditions. This was designed primarily to carry Energia rocket boosters and the Buran space shuttle from its service area to the launch site as part of the Buran Shuttle Program.Loads that are too large can be carried on a wide cargo deck and on an externally mounted mount. Cossack has an air cargo handling system and cargo door equipped with slopes to carry out loading and unloading missions quickly and easily. It is also equipped with airplane barrel extensions on the front and rear wings to increase range. Load security system installs uniquely sized payloads to the upper fuselage parts.
The aircraft is equipped with a 32 wheel landing gear system. The landing nose features four wheels on the front of the fuselage. The rear body consists of 16 wheels that can be reduced from 28 tires mounted on the main landing gear. This aircraft can turn full on a runway as wide as 60m.
Geometrical Characteristics
|
|
Length
(m)
|
84
|
Wingspan
(m)
|
88.4
|
Height
(m)
|
18.1
|
Door
dimensions (W x H) (cm)
|
640 x 440
|
Cargo
hold (L x W x H) (cm)
|
4335 x 640 x 440
|
Useable
volume (m³)
|
1300
|
Wing
area (m²)
|
905.0
|
Crew and Passengers
|
|
Crew
members
|
6
|
Passengers
|
70
|
Mass and Capacity
|
|
Dry
mass (t)
|
350
|
Maximum
weight to take off (t)
|
600
|
Payload
mass (t)
|
250
|
Motorization
|
|
Type
|
ZMKB Progress D-18
|
Number
of turbofans
|
6
|
Thrust
of each turbofan (kN)
|
229
|
Performances
|
|
Nominal
speed (km/h)
|
700
|
Maximal
speed (km/h)
|
850
|
Operating
range (empty / full) (km)
|
15400
/ 4500
|
Ceiling
(maximum / cruise) (m)
|
11145
/ 10000
|
Takeoff
run with maximum payload (m)
|
3500
|
Wing
loading (kg/m²)
|
662.9
|
Antonov An-225 Mriya Engines
The Antonov An-225 Mriya is powered by six Ivchenko Progress Lotarev D-18T, three shaft turbofan engines, each of which can produce a maximum thrust of 229.5 kN.It is equipped with bucket-shaped push-in, jetpipe, drive box, exhaust nozzle, fan turbine, combustion chamber, intermediate drive, fan stator blades and fan wheels. The length and width of the machines are 5.4 m and 2.7 m respectively. He is 2.9 m tall. The dry weight is 4,100kg. Service life is 24,000 hours.
The An-225 Mriya can fly with a maximum speed of 850 km / hour. The cruising speed is 800 km / hour. The range of aircraft varies between 4,000 km and 15,400 km.
Antonov An-225 Mriya Cabin and Cargo
A large pressure cargo compartment can carry a variety of loads. The length and width of the compartments are 43 m and 6.4 m, respectively. Height of 4.4m. Floor area and volume are 280m² and 1,300m³ respectively. The compartment can carry 250t of internal cargo or 200t to a height of 70m on the plane.This aircraft can reach non-stop intercontinental flights while accommodating 180t or 200t payload. It also can carry out intercontinental air transportation with a weight of 150 tons. It can carry 16 standard UAC-10 aeronautical containers, each weighing 10t, 50 cars, turbines, generators, dump trucks, Belaz, Kamatsu and Euclid.
I watched it take off from Williams Gateway Airport in Mesa Arizona. Beautiful
ReplyDeleteI did too, when it brought in the Transformer for either SRP or APS...I believe it was SRP.
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