| Type | Aircraft | |
| Company | SC A.S. Yakovlev Design Bureau | |
| Scheme | Midwing Monoplane | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
8.7
88.7
|
|
| Wings | ||
| Wing area (m2) |
1.1
14
925
|
|
| Wingspan (Beam) (m) |
0.1
8.9
95
|
|
| Wing loading (kg/m2) |
3.1
163
829
|
|
| Weights | ||
| Empty weight (kg) |
8
2,285
276,800
|
|
| Max. takeoff weight (Gross weight) (kg) |
154
3,535
575,000
|
|
| Capacity | ||
| Crew (per.) |
1
1
112
|
|
| Speeds | ||
| Max. Speed (km/h) |
25
982
28,165
|
|
| Power | ||
| Thrust/weight (kN/kg) |
0.0
0.5
2.1
|
|
| Thrust (kN) |
1.5
15.6
1,914
|
1 powerplant |
| Performance | ||
| Service ceiling (m) |
0.6
14,000
161,544
|
|
| Range (Ferry range) (km) |
4
1,100
40,700
|
|
| Dynamic Performance | ||
| Rate of climb (m/min) |
1.9
2,220
36,000
|
|
| Combat | ||
| Guns (qt) |
1
3
18
|
23 mm (0.906 in) Nudelman-Rikhter NR-23 cannon, 75 rpg |
| Stat | ||
| Number built (qt) |
0
1
43,000
|
|
| Introduction | 1947 | |
| First flight | 02.11.1947 | |
