|
AN-124-100 and AN-124-100M-150 Basic Performance
| |
| AN-124-100
| AN-124-100M-150
| AN-124-100M-150
| AN-124-100M-150
| | Takeoff weight, t
| 392
| 402
| 402*
| 370**
| | Maximum lift capacity, t
| 120
| 150
| 150
| 150
| |
Range, km:
| |
with 150 t of cargo
| -
| 3 200
| 3 200
| 1 450
| |
with 120 t of cargo
| 4 650
| 5 200
| 5 200
| 3 100
| |
с with 40 t of cargo
| 11 350
| 11 900
| 11 900
| 8 500
| |
without cargo
| 14 200
| 14 400
| 14 400
| 11 700
| | Flight speed, km/h
| 800 - 850
| 800 - 850
| 800 - 850
| 800 - 850
| | Flight altitude, m
| 9 000 - 11 600
| 8 800 - 11 600
| 9 100 - 11 600
| 9 100 - 11 600
| |
Engines:
| |
type
| ТРДД Д18Т III-Series
| ТРДД Д18Т III-Series
| ТРДД Д18Т IV-Series
| ТРДД Д18Т IV-Series
| |
quantity of x thrust, kN
| 4 x 23,4
| 4 x 23,4
| 4 x 25,8
| 4 x 25,8
| | Runway length, m
| 2 800
| 3 000
| 2 800
| 2 000
| | Required runway strength, R/B
| 43,7
| 45,0
| 45,0
| 41,5
| |
Cargo compartment dimensions, m:
| |
floor length (with the ramps)
| 36,5 (43,7)
| 36,5 (43,7)
| 36,5 (43,7)
| 36,5 (43,7)
| |
width (across the floor)
| 6,4
| 6,4
| 6,4
| 6,4
| |
height
| 4,4
| 4,4
| 4,4
| 4,4
| | Cargo compartment volume, m3
| 1160
| 1160
| 1160
| 1160
| | Crew, prs.
| 6
| 4
| 4
| 4
|
* the increase of maximal take-off weight till 420 t is foreseen
** characteristics when operating from runway with length 2000 m |
