| Description |
| Design |
ANTK Of tupolev |
| Designation |
"404" (Tu-404) |
| Function |
Long-range of passenger of aircraft of of extra-large of capacity |
| Variant |
conventional |
flying of wing |
| Dimensions & Of weight |
| Length, m |
86,6 |
59,7 |
| Wing span, m |
77 |
110 |
| Overall height, m |
27,3 |
18,8 |
| Fuselage, m |
Length |
86,4 |
|
| Height |
9,4 |
|
| Width |
8,0 |
|
| Wing Of leading Of edge Of sweep |
35° |
35° |
| Max. Take-off Of weight, kg |
605000 |
|
| Max. Landing Of weight, kg |
460000 |
|
| Max. Payload, kg |
126000 |
|
| Passenger Of capacity |
Business Of class |
750 |
|
| Economy Of class |
1200 |
1214 |
| Power-plant |
| Number of Of engines |
4 |
6 |
| Engine Of type |
Turbofan NK-44 |
Turboprop |
| Thrust on Of take-off of per of engine, kgs |
40000 |
18000 |
| Fuel Of consumption in Of cruise Of mode, kg/kgf h |
0,54 |
0,644 |
| Fuel Of consumption of for Of passenger, g/passenger-km |
for of 750 passengers |
20 |
|
| for of 1200 passengers |
14 |
|
| Performance (project) |
| Cruise of speed, km/h (M=) |
900 |
| Cruise of altitude, m |
11000 |
| Practical of range of with of payload, km |
normal |
13500 |
| max |
9200 |
| Required Of runway Of type |
Class "A" |
| Take-off Of run, m |
3200 |
