Type | Aircraft | |
Company | SC A.S. Yakovlev Design Bureau | |
Scheme | Monoplane High wing | |
Geometry | ||
---|---|---|
Length (m) |
1.9
8
88.7
|
|
Height (m) |
0.6
2.5
50.1
|
tail up |
Wings | ||
Wing area (m2) |
1.1
23
925
|
|
Wingspan (Beam) (m) |
0.1
12.8
95
|
|
Weights | ||
Empty weight (kg) |
8
670
276,800
|
|
Max. takeoff weight (Gross weight) (kg) |
154
912
575,000
|
|
Capacity | ||
Crew (per.) |
1
1
112
|
|
Capacity passengers (per.) |
1
3
400
|
|
Speeds | ||
Max. Speed (km/h) |
25
192
28,165
|
|
Сruise Speed (km/h) |
52
152
3,087
|
|
Power | ||
Total Power (hp) |
0.4
200
60,000
|
1 powerplant |
Performance | ||
Service ceiling (m) |
0.6
4,275
161,544
|
|
Dynamic Performance | ||
Time to altitude (min) |
0.6
6.5
105
|
to 1000 m |
Stat | ||
Number built (qt) |
0
1
43,000
|
|
First flight | 1931 |