| | SB-2M100A:
|
| Development | TsAGI of Arkhangelsk A.A./Tupolev A.N.
|
| Manufacturers | Plants #22 (Moscow), #125 (Irkutsk)
|
| Issue (PCs.) | 6831? (6656?)
|
| Years (Development-tests) | 1934-40 |
| Years (first flight) | 1934 |
| Years (production) | 1936-41 |
| length of the aircraft | 12.27-12.57 m
|
| wing span | 20.33 m
|
| height | 4,735 m
|
| wing area | 56.00-56.7 square meters
|
| Weight empty (kg.) | 4768
|
| normal take-off weight | 5732 kg
|
| Weight takeoff (kg.) | 7880
|
| bomb load | 500/600 kg
|
| Engine (Power (HP) | 2 x M-103 (960)
|
| Speed Cruise (km/h) | 375
|
| maximum speed at an altitude of 4000 m | 423 km / h
|
| Speed Max (km/h) | 450
|
| Climb (M/min) | 570
|
| Practical Ceiling (m) | 7800-9560 m
|
| Flight Range | 1500-2300 km
|
| Armament: cannon, machine-gun | 4-6 x 7.62mm ShKAS
|
| Bombs (kg.) | 600.
|
| crew | 3 people
|
