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 |