Tu-330
Main perfomance of baseline Tu-204-330 version with PS-90A and NK-93A engines |
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engines, number, type, take-off thrust, kgf |
PS-90A
(2 x 16140) |
NK-93A
(2 x 20000) |
Geometric data
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wing span, m |
43,70
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a/c lenght, m |
42,7
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a/c height, m |
14,50
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wing area, sq.m |
196,55
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cargo compartment size (length x, width x, height x) |
23,5 õ 4,0 õ 4,0 (3,55 under center wing)
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actual capacity of cargo comprtment, cub. m |
350
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floor area, sq.m |
96
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Weights and loads
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max take-off weight from concrete runway, t |
103,5
|
112,0
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max carried payload from concrete runway, t |
35
|
35
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from unpaved runway, t |
20
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25
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fright range from concrete runway of 2200m lenght | ||
at payload of 35t, km |
1800
|
3200
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30 t, km |
3000
|
4200
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25 t, km |
4400
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5800
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20 t, km |
5700
|
7000
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ferry, km |
8800
|
9500
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cruise speed, km/h |
800-850
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cruise altitude, m |
11000
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12000
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RWY lenght required, m |
2200
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min RWY subsoil strength, kgf/sq |
6,0-7,0
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fuel flow rate per 1 hour of flight, t |
3,5
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3,1
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specific fuel consumpsion for service range at max payload, g/t-km |
138-140
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118-122
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Operating characteristics
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assigned service life, t.h. |
45000
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maintenance and repair ground time, h/f.h. |
at most 0,7
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turn round time, min |
30
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Description | Lockhead C-130J |
Tupolev TU-330 (TU-204-330) |
Airbus A-400M |
Crew size | 3 | 3 | 3 |
Wing area (m2) | 162.12 | 196.55 | 221.5 |
Max Take-off weight (t) | 79.4 | 112 | 130 |
Max payload (t) | 21.69 | 35 | 37 |
Engines: type thrust (kg) Power (h.p) |
Turboprop AE2100D 4 x (6000) |
Propfan NK-93 2 x 18000 |
Turboprop 4 x (10000) |
Flight range (km): at typical payload at max payload |
5245 (15.875 t) ~4000 |
5600 (25 t) 3000 |
5600 (25 T) 3150 |
Fuel efficiency (g/t-km) | 150 | 118-122 | 145 |
Max cruising flight speed (M number), km/h | 600 | 850 | 780 |
Geometric data: wing span (m) A/c length (m) A/c height (m) |
40.41 34.37 11.66 |
43.7 41.76 14.5 |
42.5 42.2 14.7 |
Cargo compartment: cargo compartment capacity (m3) cargo compartment (m) floor area (m2) |
123.2 - 49 |
350 23.5 96 |
356 22.5 92 |
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