*****AIRCRAFT “Antonov - AN225”*****

REFERENCE INFORMATION (by Aircraft performance database)

 

*****Aircraft Features*****

Wing position:  High wing

Engine position: Underwing mounted

Tail configuration: Double fin, low set

Landing gear: Tricycle retractable

Wing Span: 88.4 m (290 ft.)

Length:     84 m (275 ft.)

Height:     18.2 m (59.3 ft)

Power plant: 6 x 229.5 kN Lotarev D-18T turbofans,

229.5 kN (51,600 lbf) each 

Accommodation: Flightcrew of six and up to 70 passengers in upper deck.

Notes: Ultra heavy lift transport aircraft.

The Antonov 225 first flew in December 1988 and entered service

from 1989 to 1994. World´s largest aircraft, designed to participate

in the soviet space program. Only 1 aircraft was built.

From mid 2001, the aircraft was restored and re-entered service

with Antonov Design Bureau.
Alternative names:
ANTONOV An-225 Mriya, Mriya
.

 

*****Total Flight Simulator aircraft weight with full fuel*****  

600,000 kg (1,322,770 lb.)

VMO - Maximum Operating Speed 000 KIAS

MMO - Maximum Operating Speed Mach  0.00 Mach

Turbulent Air Penetration Speed   000 KIAS/.00 Mach

VLO - Maximum Gear Operating Speed   000 KIAS

VLE - Maximum Landing Gear Extension Speed   000 KIAS/.00 Mach

 

*****Maximum Flap Placard Speeds*****

Flaps degrees     KIAS

1           000

2           000

5           000

10          000

15          000

25          000

30          000

40          000

 

*****Take-off*****

WTC:        H

Distance:   3500 mt

V2 (IAS):   195 kts

 

*****Climbing*****

-(to 5000 ft)

IAS:        250 kt

ROC:        170 ft/min

-(to FL150)

IAS:        330 kt

ROC:        1900 ft/min

-(to FL240)

IAS:        330 kt

ROC:        1900 ft/min

-(mach)

mach:       0.78

ROC:        650 ft/min

 

*****Cruise*****

TAS:        800 km/h (430 knots, 500 mph)

            MAX 850 km/h (460 knots, 530 mph) 

MACh:       0.78

Ceiling:    FL450

Range:      3000 NM

 

*****Descent *****

- (to FL240)

mach:       0.78

ROD:        1500 ft/min

- (to FL100)

IAS:        330 kt

ROD:        2200 ft/min

 

*****Approach*****

IAS:        250 kt

MCS:        230 kt

ROD:        1500 ft/min

 

*****Landing*****

Vht (IAS):  150 kt

APC:        C

Distance:   nd mt