| Type | Aircraft | |
| Company | Lockheed Corporation | |
| Scheme | Integrated Monoplane | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
14.4
88.7
|
|
| Height (m) |
0.6
2.3
50.1
|
|
| Wings | ||
| Wing area (m2) |
1.1
35.9
925
|
|
| Wingspan (Beam) (m) |
0.1
6.9
95
|
|
| Weights | ||
| Empty weight (kg) |
8
4,059.7
276,800
|
|
| Max. takeoff weight (Gross weight) (kg) |
154
5,669.9
575,000
|
|
| Capacity | ||
| Crew (per.) |
1
1
112
|
|
| Speeds | ||
| Max. Speed (km/h) |
25
966
28,165
|
|
| Сruise Speed (km/h) |
52
456
3,087
|
|
| Fuel | ||
| Fuel Capacity (l) |
23
1,588
320,000
|
|
| Power | ||
| Thrust/weight (kN/kg) |
0.0
0.5
2.1
|
0.46–0.62 |
| Thrust (kN) |
1.5
13.1
1,914
|
|
| Performance | ||
| Service ceiling (m) |
0.6
10,200
161,544
|
|
| Endurance (h) |
0.0
1
150
|
|
| Stat | ||
| Number built (qt) |
0
2
43,000
|
|
| Introduction | 1977 | |
| First flight | 01.12.1977 | |
| Stop production | 1979 | |
