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Ò-4
Data
SZ-2 prototype April 1938
BB-1 prototype April 1939
BB-1 prototype April 1940
Su-2 No16/2, 20/2 January 1941
Engine
M-62
M-87A
M-88B
M-88B
Takeoff weight, normal, kg
3,670
4,030
4,121
4,345
Dead weight, kg
-
2,850
2,875
2,970
Maximum speed at sea level, kph
360
375
375
378
Maximum speed (kph)/at height (m)
403/4,700
468/5,200
467/6,600
455/4,400
Service ceiling, m
7,440
8,800
8,900
8,900
Flight range, km
-
1,160
810
1,090
Takeoff run, m
380
270-290
-
388
Landing run, m
240
260-280
-
452
Aircraft length, mm
9,915
10,250
10,250
10,250
Aircraft height, flight alignment, mm
3,930
3,940
3,940
3,940
Wingspan, mm
14,370
14,300
14,300
14,300
Armaments
6xShKAS
6xShKAS
5xShKAS
5xShKAS
Bomb load, norm/max, kg
200/800
200/400
400/600
400/-
Data
Su-2 No 1/6 mod.
production
March 1941
Su-2 No 13,016
prototype
June 1941
Su-2
Production
July 1941
Su-2 No 15,116
Production
April 1942
Engine
M-88B
M-89
M-88B
M-82
Takeoff weight, normal, kg
4,310
4,005
4,335
4,700
Dead weight, kg
2,954
-
2,995
3,213
Maximum speed at sea level, kph
410
429
370
430
Maximum speed (kph)/at height (m)
512/7,100
522/6,975
455/6,700
486/5,800
Service ceiling, m
9,120
-
8,500
8,400
Flight range, km
1,180
673(P)
-
790
Takeoff run, m
474
-
460
450
Landing run, m
425
-
547
-
Aircraft length, mm
10,250
10,250
10,250
-
Aircraft height, flight alignment, mm
3,940
3,940
3,940
3,940
Wingspan, mm
14,300
14,300
14,300
14,300
Armaments
3xShKAS
3xShKAS
3xShKAS
6xShKAS
Bomb load, norm/max, kg
400/600
400/600
400/600
400/-
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