| Type | Aircraft | |
| Company | Nakajima Aircraft Company | |
| Scheme | Parasol Monoplane | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
7.3
88.7
|
|
| Height (m) |
0.6
2.8
50.1
|
|
| Wings | ||
| Wing area (m2) |
1.1
20
925
|
|
| Wingspan (Beam) (m) |
0.1
11
95
|
|
| Weights | ||
| Empty weight (kg) |
8
1,075
276,800
|
|
| Loaded weight (kg) |
5
1,530
242,500
|
|
| Capacity | ||
| Crew (per.) |
1
1
112
|
|
| Speeds | ||
| Max. Speed (km/h) |
25
300
28,165
|
|
| Сruise Speed (km/h) |
52
268
3,087
|
|
| Power | ||
| Total Power (hp) |
0.4
520.1
60,000
|
1 powerplant |
| Performance | ||
| Service ceiling (m) |
0.6
9,000
161,544
|
|
| Endurance (h) |
0.0
2
150
|
|
| Dynamic Performance | ||
| Rate of climb (m/min) |
1.9
750
36,000
|
|
| Time to altitude (min) |
0.6
4
105
|
to 3000 m |
| Combat | ||
| Guns (qt) |
1
2
18
|
fixed, forward-firing 7.7 mm (.303 in) machine guns |
| Stat | ||
| Number built (qt) |
0
450
43,000
|
|
| Introduction | 1931 | |
| First flight | 1931 | |
| Stop production | 1937 | |
