| Type | Aircraft | |
| Company | SC A.S. Yakovlev Design Bureau | |
| Scheme | Low wing Monoplane | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
10.1
88.7
|
|
| Height (m) |
0.6
3.4
50.1
|
|
| Wings | ||
| Wing area (m2) |
1.1
14.3
925
|
|
| Wingspan (Beam) (m) |
0.1
9.4
95
|
|
| Wing loading (kg/m2) |
3.1
154
829
|
|
| Weights | ||
| Empty weight (kg) |
8
1,555
276,800
|
|
| Max. takeoff weight (Gross weight) (kg) |
154
2,550
575,000
|
|
| Capacity | ||
| Crew (per.) |
1
2
112
|
student and instructor |
| Useful load (kg) |
26.4
991
90,700
|
|
| Speeds | ||
| Max. Speed (km/h) |
25
660
28,165
|
|
| Сruise Speed (km/h) |
52
548
3,087
|
|
| Fuel | ||
| Fuel Capacity (l) |
23
1,006
320,000
|
|
| Power | ||
| Thrust/weight (kN/kg) |
0.0
0.4
2.1
|
|
| Thrust (kN) |
1.5
8.8
1,914
|
1 powerplant |
| Performance | ||
| Service ceiling (m) |
0.6
16,127.9
161,544
|
|
| Range (Ferry range) (km) |
4
965
40,700
|
|
| Takeoff roll (m) |
20
425
3,200
|
|
| Landing roll (m) |
20
450
2,570
|
|
| Dynamic Performance | ||
| Rate of climb (m/min) |
1.9
1,080
36,000
|
|
| Stat | ||
| Number built (qt) |
0
4
43,000
|
|
| Introduction | 1960 | |
| First flight | 20.05.1960 | |
