| Type | Aircraft | |
| Company | Mitsubishi Aircraft Corporation | |
| Scheme | Monoplane High wing | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
17.9
88.7
|
|
| Height (m) |
0.6
4.5
50.1
|
|
| Wings | ||
| Wing area (m2) |
1.1
21.2
925
|
|
| Wingspan (Beam) (m) |
0.1
7.9
95
|
|
| Wing loading (kg/m2) |
3.1
645
829
|
|
| Weights | ||
| Empty weight (kg) |
8
6,358
276,800
|
|
| Max. takeoff weight (Gross weight) (kg) |
154
13,674
575,000
|
|
| Capacity | ||
| Crew (per.) |
1
1
112
|
|
| Hardpoints (qt) |
1
7
2,576
|
One, centerline, four underwing and two wingtip missile rails |
| Speeds | ||
| Max. Speed (km/h) |
25
1,700
28,165
|
at 11000 m |
| Power | ||
| Afterburning thrust (kN/kg) |
29.4
71.2
980
|
2 powerplants 35,6 each |
| Thrust (kN) |
1.5
45.6
1,914
|
2 powerplants 22,8 each |
| Performance | ||
| Service ceiling (m) |
0.6
15,240
161,544
|
|
| Range (Ferry range) (km) |
4
2,870
40,700
|
with max external fuel |
| Сombat radius (km) |
277
556
7,210
|
High-Low-High profile with two ASM-1 missiles and one 830 L drop tank |
| Dynamic Performance | ||
| Rate of climb (m/min) |
1.9
7,080
36,000
|
|
| Time to altitude (min) |
0.6
2
105
|
to 11000 m |
| Combat | ||
| Guns (qt) |
1
1
18
|
20 mm (0.787 in) JM61A1 Vulcan 6-barreled Gatling cannon |
| Stat | ||
| Number built (qt) |
0
77
43,000
|
|
| Introduction | 1975 | |
| First flight | 03.06.1975 | |
| Stop production | 01.03.2006 | |
