Type | Aircraft | |
Company | Mitsubishi Aircraft Corporation | |
Scheme | Integrated Monoplane | |
Geometry | ||
---|---|---|
Length (m) |
1.9
6.0
88.7
|
|
Height (m) |
0.6
2.7
50.1
|
|
Wings | ||
Wing area (m2) |
1.1
17.7
925
|
|
Wingspan (Beam) (m) |
0.1
9.5
95
|
|
Wing loading (kg/m2) |
3.1
219.2
829
|
|
Weights | ||
Empty weight (kg) |
8
1,445
276,800
|
|
Max. takeoff weight (Gross weight) (kg) |
154
3,870
575,000
|
|
Loaded weight (kg) |
5
3,000
242,500
|
|
Capacity | ||
Crew (per.) |
1
1
112
|
|
Speeds | ||
Max. Speed (km/h) |
25
900
28,165
|
at 10000 m |
Сruise Speed (km/h) |
52
699
3,087
|
|
Stall Speed (km/h) |
40
150
257.7
|
|
Power | ||
Thrust/weight (kN/kg) |
0.0
0.4
2.1
|
|
Thrust (kN) |
1.5
17.5
1,914
|
1 powerplant |
Performance | ||
Service ceiling (m) |
0.6
12,000
161,544
|
|
Dynamic Performance | ||
Rate of climb (m/min) |
1.9
3,000
36,000
|
|
Time to altitude (min) |
0.6
0.7
105
|
to 2000 m |
0.6
2.1
105
|
to 4000 m | |
0.6
3.1
105
|
to 8000 m | |
0.6
3.8
105
|
to 10000 m | |
Combat | ||
Guns (qt) |
1
2
18
|
Type 5 30mm cannon with 53 rounds per gun |
Stat | ||
Number built (qt) |
0
7
43,000
|
|
Introduction | 1945 | |
First flight | 07.07.1945 |