Type | Aircraft | |
Company | Mitsubishi Aircraft Corporation | |
Scheme | Low wing Monoplane | |
Geometry | ||
---|---|---|
Length (m) |
1.9
10.5
88.7
|
|
Height (m) |
0.6
2.9
50.1
|
|
Wings | ||
Wing area (m2) |
1.1
31.5
925
|
|
Wingspan (Beam) (m) |
0.1
15.9
95
|
|
Wing loading (kg/m2) |
3.1
91
829
|
|
Weights | ||
Empty weight (kg) |
8
1,840.2
276,800
|
|
Max. takeoff weight (Gross weight) (kg) |
154
2,860
575,000
|
|
Loaded weight (kg) |
5
2,857.6
242,500
|
|
Capacity | ||
Crew (per.) |
1
1
112
|
pilot |
Capacity passengers (per.) |
1
6
400
|
|
Speeds | ||
Max. Speed (km/h) |
25
338.0
28,165
|
at 2230 m |
Сruise Speed (km/h) |
52
309.0
3,087
|
at 75% power and 2230 m |
Power | ||
Power/mass (hp/kg) |
0.0
0.2
22.1
|
|
Total Power (hp) |
0.4
690
60,000
|
2 powerplants 345 hp each |
Performance | ||
Service ceiling (m) |
0.6
6,858
161,544
|
|
Range (Ferry range) (km) |
4
1,046
40,700
|
at 62.5% power and 3050 m |
Dynamic Performance | ||
Rate of climb (m/min) |
1.9
250
36,000
|
|
Time to altitude (min) |
0.6
8
105
|
to 3050 m |
Stat | ||
Number built (qt) |
0
11
43,000
|
|
Introduction | 1934 | |
First flight | 26.06.1934 | |
Stop production | 1951 |