| 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 | |
