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Antonov

An-225 Mriya

CARGO


Type:
Turbofan airplane

Origin:
Country FlagUkraine
Manufacturer:
1985–

Updated March 8, 2024
Aircraft picture
An-225 Mriya - Olivier CABARET. CC-BY-2.0

General characteristics (13)

  • Role
    Cargo
  • Body
    Wide
  • Wing
    Fixed wing
  • Wing position
    High wing
  • Tail
    Double fin, low set
  • WTC
    H
  • Type code
    L6J
  • Landing gear
    Quadricycle retractable
  • Crew
    6
  • Payload capacity
    250,000kg (551,155lbs)
  • Engine count
    6
  • ICAO type designator
    A225
  • Engine position
    Underwing mounted

Structural data (13)

  • Length
    84 m (275.59 ft)
  • Height (overall)
    18.2 m (59.71 ft)
  • Wingspan
    88.4 m (290 ft 0 in)
  • Aspect ratio
    8.6
  • Wing area
    905 m² (9,741.42 sq ft)
  • Wing loading
    662.9 kg/m2 (135.8lb/ft2)
  • Cargo compartment L.
    43.3 m (142 ft)
  • Cargo compartment W.
    6.4 m (21 ft)
  • Cargo compartment H.
    4.4 m (14 ft 5 in)
  • Cargo compartment Vol.
    1,220 m³ (43,084 cuft)
  • Cargo door W.
    6.4 m (251.9 in)
  • Cargo door H.
    4.4 m (173.2 in)
  • On-board crane
    30,000 kg lift (66,139 lbs)

Performance (3)

  • Range
    15,400 km (9,600 mi, 8,300 nmi) with maximum fuel; range with 200 tonnes payload: 4,000 km (2,500 mi)
  • Fuel capacity
    464,516 L (122,711 US gal)
  • Service ceiling
    11,610 m (38,100 ft)

Speeds (7)

  • Flaps extended (VFE)
    200 kt (370 km/h)
  • Gear extended (VGE)
    248 kt (459 km/h)
  • Gear operating (VGO)
    248 kt (459 km/h)
  • Operating (VOP)
    308 kt (570 km/h)
  • Maximum (normal)
    850 km/h (530 mph, 460 kt)
  • Cruise (normal)
    800 km/h (500 mph, 430 kt)
  • Operating Mach
    0.77

Indicative Flight Profile data (23)
Source:SKYbrary logoSKYbrary [1]

  • Takeoff
    V2: 195 kts
    Distance: 2500 m
    Weight: 640000 kg
  • Initial climb (to 5000 ft)
    IAS: 250 kts
    ROC: 1700 ft/min
  • Initial climb (to 15,000 ft)
    IAS: 330 kts
    ROC: 1900
  • Initial climb (to 24,000 ft)
    IAS: 330 kts
    ROC: 1900 ft/min
  • Mach climb
    Mach: 0,78
    ROC: 650 ft/min
  • Cruise
    TAS: 458 kts
    Mach: 0,78
    Ceiling: FL450
    Range: 2425 NM
  • Initial descent (to 24,000 ft)
    IAS: 0,78
    ROD: 1500 ft/min
  • Descent (to 10,000 ft)
    IAS: 330 kts
    ROD: 2200 ft/min
  • Descent (below 10,000 ft)
    IAS: 250 kts
    MCS: 230 kts
    ROD: 1500 ft/min
  • Approach
    VAPP (IAS): 150 kts
    Distance: -

Weights (3)

  • MLW
    550,000 kg (1,212,540 lb)
  • MTOW
    640,000 kg (1,410,960 lb)
  • MTW
    650,000 kg (1,433,000 lb)

Engine options (1)

  • Model
    Progress D-18T
  • Manufacturer
    Country FlagMotor Sich
  • Type
    Turbofan
  • Engine count
    6
  • Length
    5.4 m (212.6 in)
  • Width
    2.93 m (115.6 in)
  • Height
    2.79 m (109.9 in)
  • Fan diameter
    2.33 m (91.73 in)
  • Dry weight
    4,100 kg (9,039 lb)
  • Thrust-to-weight ratio
    5.72
  • Max thrust
    Takeoff: 23,430 kgf (51,700 lbf; 229.8 kN); Cruise: 4,860 kgf (10,700 lbf; 47.7 kN)
  • Bypass ratio
    5.7
  • Pressure ratio
    27.5
  • SFC
    Takeoff: 9.8 g/(kNs) (0.345 lb/(lbfh)); Cruise: 15.5 g/(kNs) (0.546 lb/(lbfh))
  • Compressor
    Axial, 7xIP, 7xHP
  • Turbine
    1xHP, 1xIP, 4xLP
  • Combustors
    Annular

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