Type | Aircraft | |
Company | Joint Stock Company Tupolev | |
Scheme | Low wing Monoplane | |
Geometry | ||
---|---|---|
Length (m) |
1.9
13.2
88.7
|
|
Height (m) |
0.6
5.5
50.1
|
|
Wings | ||
Wing area (m2) |
1.1
55.1
925
|
|
Wingspan (Beam) (m) |
0.1
19.2
95
|
|
Weights | ||
Empty weight (kg) |
8
3,900
276,800
|
|
Max. takeoff weight (Gross weight) (kg) |
154
5,300
575,000
|
|
Loaded weight (kg) |
5
5,300
242,500
|
|
Capacity | ||
Crew (per.) |
1
3
112
|
|
Speeds | ||
Ground Speed (km/h) |
96.6
296
1,500
|
|
Max. Speed (km/h) |
25
352
28,165
|
|
Сruise Speed (km/h) |
52
321
3,087
|
|
Fuel | ||
Fuel Capacity (l) |
23
1,072
320,000
|
|
Power | ||
Total Power (hp) |
0.4
2,038
60,000
|
2 powerplants 1019 hp each |
Performance | ||
Service ceiling (m) |
0.6
9,170
161,544
|
|
Dynamic Performance | ||
Rate of climb (m/min) |
1.9
526
36,000
|
|
Combat | ||
Guns (qt) |
1
3
18
|
1 moveable machine gun; 2 recoilless cannon |
Stat | ||
Number built (qt) |
0
1
43,000
|
|
Introduction | 1935 | |
First flight | 01.02.1935 |