Type | Aircraft | |
Company | Nakajima Aircraft Company | |
Scheme | Monoplane Low wing | |
Geometry | ||
---|---|---|
Length (m) |
1.9
11.8
88.7
|
|
Height (m) |
0.6
4.5
50.1
|
|
Wings | ||
Wing area (m2) |
1.1
26
925
|
|
Wingspan (Beam) (m) |
0.1
13.4
95
|
|
Wing loading (kg/m2) |
3.1
216.6
829
|
|
Weights | ||
Empty weight (kg) |
8
4,388
276,800
|
|
Max. takeoff weight (Gross weight) (kg) |
154
6,102
575,000
|
|
Loaded weight (kg) |
5
5,633
242,500
|
|
Capacity | ||
Crew (per.) |
1
1
112
|
|
Speeds | ||
Max. Speed (km/h) |
25
697
28,165
|
|
Сruise Speed (km/h) |
52
470
3,087
|
|
Power | ||
Total Power (hp) |
0.4
2,400
60,000
|
1 powerplant |
Performance | ||
Service ceiling (m) |
0.6
12,855
161,544
|
|
Range (Ferry range) (km) |
4
1,200
40,700
|
|
Combat | ||
Guns (qt) |
1
4
18
|
2 × 30 mm (1.18 in) Ho-105 cannons in the outer wing panels and 2 × 20 mm synchronized Ho-5 cannons in the wing roots |
Bombs (qt) |
1
1
250
|
250 kg (550 lb) bomb under fuselage |
Stat | ||
Number built (qt) |
0
1
43,000
|
|
Introduction | 1945 | |
First flight | 01.04.1945 |