| Type | Aircraft | |
| Company | Lockheed Corporation | |
| Scheme | High wing Monoplane | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
17.5
88.7
|
|
| Height (m) |
0.6
5.2
50.1
|
|
| Wings | ||
| Wingspan (Beam) (m) |
0.1
8.9
95
|
|
| Weights | ||
| Empty weight (kg) |
8
8,112
276,800
|
|
| Max. takeoff weight (Gross weight) (kg) |
154
15,900
575,000
|
|
| Capacity | ||
| Crew (per.) |
1
1
112
|
|
| Speeds | ||
| Max. Speed (km/h) |
25
2,720
28,165
|
|
| Power | ||
| Afterburning thrust (kN/kg) |
29.4
111.2
980
|
1 powerplant |
| Thrust (kN) |
1.5
66.7
1,914
|
1 powerplant |
| Performance | ||
| Service ceiling (m) |
0.6
18,300
161,544
|
more than 18300 |
| Range (Ferry range) (km) |
4
3,400
40,700
|
with 8800 kg |
| Takeoff roll (m) |
20
440
3,200
|
|
| Landing roll (m) |
20
930
2,570
|
|
| Dynamic Performance | ||
| Rate of climb (m/min) |
1.9
18,000
36,000
|
|
| Stat | ||
| Introduction | 1968 | |
