Type | Aircraft | |
Company | Kawasaki Heavy Industries | |
Scheme | Midwing Monoplane | |
Geometry | ||
---|---|---|
Length (m) |
1.9
29.2
88.7
|
|
Height (m) |
0.6
8.9
50.1
|
|
Wings | ||
Wing area (m2) |
1.1
92.9
925
|
|
Wingspan (Beam) (m) |
0.1
30.9
95
|
|
Weights | ||
Empty weight (kg) |
8
19,278
276,800
|
|
Max. takeoff weight (Gross weight) (kg) |
154
34,020
575,000
|
|
Capacity | ||
Crew (per.) |
1
12
112
|
2 pilots + 10 operators |
Speeds | ||
Max. Speed (km/h) |
25
650
28,165
|
|
Сruise Speed (km/h) |
52
402
3,087
|
|
Fuel | ||
Fuel Capacity (l) |
23
12,946
320,000
|
|
Power | ||
Total Power (hp) |
0.4
5,700
60,000
|
2 powerplants 2850 hp each |
Thrust (kN) |
1.5
27.4
1,914
|
2 powerplants 13,7 kN each |
Performance | ||
Service ceiling (m) |
0.6
9,150
161,544
|
|
Range (Ferry range) (km) |
4
4,445
40,700
|
|
Dynamic Performance | ||
Rate of climb (m/min) |
1.9
548
36,000
|
|
Propellers | ||
Propellers (qt) |
1
2
8
|
|
Prop blade number (qt) |
1
3
8
|
|
Combat | ||
Bombs weight (kg) |
2
3,629
39,000
|
including free-fall bombs, depth charges, and torpedoes |
Stat | ||
Number built (qt) |
0
83
43,000
|
|
Introduction | 1966 | |
First flight | 21.07.1966 | |
Stop production | 1996 |