| Type | Aircraft | |
| Company | Mitsubishi Aircraft Corporation | |
| Scheme | Monoplane Parasol | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
8.5
88.7
|
|
| Height (m) |
0.6
3.5
50.1
|
|
| Wings | ||
| Wingspan (Beam) (m) |
0.1
12.8
95
|
|
| Wing loading (kg/m2) |
3.1
68.1
829
|
|
| Weights | ||
| Empty weight (kg) |
8
1,060
276,800
|
|
| Loaded weight (kg) |
5
1,770
242,500
|
|
| Capacity | ||
| Crew (per.) |
1
2
112
|
|
| Speeds | ||
| Max. Speed (km/h) |
25
221
28,165
|
|
| Power | ||
| Total Power (hp) |
0.4
475
60,000
|
1 powerplant |
| Performance | ||
| Service ceiling (m) |
0.6
5,700
161,544
|
|
| Endurance (h) |
0.0
5
150
|
4-5 hours |
| Dynamic Performance | ||
| Time to altitude (min) |
0.6
10.5
105
|
to 3000 m |
| Combat | ||
| Guns (qt) |
1
4
18
|
2 × fixed forward firing 7.7 mm (.303 in) machine guns, 2 × flexibly mounted machine guns in rear cockpit |
| Stat | ||
| Number built (qt) |
0
234
43,000
|
4 prototypes + 230 production aircraft |
| Introduction | 1930 | |
| First flight | 28.03.1931 | |
