Type | Aircraft | |
Company | Open Joint Stock Company «Ilyushin Aviation Complex» | |
Scheme | Low wing Monoplane | |
Geometry | ||
---|---|---|
Length (m) |
1.9
11.6
88.7
|
|
Height (m) |
0.6
4.2
50.1
|
|
Wings | ||
Wing area (m2) |
1.1
38.5
925
|
|
Wingspan (Beam) (m) |
0.1
14.6
95
|
|
Wing loading (kg/m2) |
3.1
160
829
|
|
Weights | ||
Empty weight (kg) |
8
4,360
276,800
|
|
Max. takeoff weight (Gross weight) (kg) |
154
6,380
575,000
|
|
Capacity | ||
Crew (per.) |
1
2
112
|
pilot and rear gunner |
Speeds | ||
Ground Speed (km/h) |
96.6
370
1,500
|
|
Max. Speed (km/h) |
25
414
28,165
|
|
Сruise Speed (km/h) |
52
384
3,087
|
|
Power | ||
Total Power (hp) |
0.4
1,722.5
60,000
|
1 powerplant |
Performance | ||
Service ceiling (m) |
0.6
5,500
161,544
|
|
Range (Ferry range) (km) |
4
720
40,700
|
|
Dynamic Performance | ||
Rate of climb (m/min) |
1.9
624
36,000
|
|
Combat | ||
Guns (qt) |
1
5
18
|
2 × fixed forward-firing 23 mm caliber VYa-23 cannons, 150 rounds per gun; 2 × fixed forward-firing 7.62 mm ShKAS machine guns, 750 rounds per gun; 1 × manually aimed 12.7 mm Berezin UBT machine gun in rear cockpit, 300 rounds |
Rockets (qt) |
1
12
76
|
8 × RS-82 rockets; 4 × RS-132 rockets |
Bombs weight (kg) |
2
600
39,000
|
|
Stat | ||
Number built (qt) |
0
36,183
43,000
|
|
Introduction | 1942 | |
First flight | 02.10.1939 | |
Stop production | 1954 |