Type | Aircraft | |
Company | Joint Stock Company Tupolev | |
Scheme | Midwing Monoplane | |
Geometry | ||
---|---|---|
Length (m) |
1.9
13.8
88.7
|
|
Height (m) |
0.6
4.1
50.1
|
|
Wings | ||
Wing area (m2) |
1.1
48.8
925
|
|
Wingspan (Beam) (m) |
0.1
18.9
95
|
|
Weights | ||
Empty weight (kg) |
8
7,601
276,800
|
|
Max. takeoff weight (Gross weight) (kg) |
154
11,768
575,000
|
|
Capacity | ||
Crew (per.) |
1
4
112
|
|
Speeds | ||
Ground Speed (km/h) |
96.6
420
1,500
|
|
Max. Speed (km/h) |
25
610
28,165
|
|
Сruise Speed (km/h) |
52
442
3,087
|
|
Fuel | ||
Fuel Capacity (l) |
23
2,200
320,000
|
|
Power | ||
Total Power (hp) |
0.4
3,800
60,000
|
2 powerplants |
Performance | ||
Service ceiling (m) |
0.6
9,000
161,544
|
|
Range (Ferry range) (km) |
4
2,020
40,700
|
|
Dynamic Performance | ||
Rate of climb (m/min) |
1.9
492
36,000
|
|
Stat | ||
Number built (qt) |
0
2,257
43,000
|
|
Introduction | 1946 | |
First flight | 29.01.1941 |