Type | Aircraft | |
Company | Kawasaki Heavy Industries | |
Scheme | Midwing Monoplane | |
Geometry | ||
---|---|---|
Length (m) |
1.9
13
88.7
|
|
Height (m) |
0.6
4.6
50.1
|
|
Wings | ||
Wing area (m2) |
1.1
21
925
|
|
Wingspan (Beam) (m) |
0.1
9.9
95
|
|
Weights | ||
Empty weight (kg) |
8
3,790
276,800
|
|
Max. takeoff weight (Gross weight) (kg) |
154
7,500
575,000
|
|
Capacity | ||
Crew (per.) |
1
2
112
|
two pilots in tandem |
Hardpoints (qt) |
1
2
2,576
|
|
Speeds | ||
Max. Speed (km/h) |
25
1,038
28,165
|
|
Fuel | ||
Fuel Capacity (l) |
23
2,241
320,000
|
|
Power | ||
Thrust (kN) |
1.5
32
1,914
|
2 powerplants 16 kN each |
Performance | ||
Service ceiling (m) |
0.6
15,240
161,544
|
|
Range (Ferry range) (km) |
4
1,670
40,700
|
|
Сombat radius (km) |
277
1,297
7,210
|
|
Dynamic Performance | ||
Load factor from (G) |
2
7.3
9
|
|
Rate of climb (m/min) |
1.9
3,048
36,000
|
|
Stat | ||
Introduction | 1985 | |
First flight | 29.07.1985 |