| Type | Aircraft | |
| Company | Lockheed Corporation | |
| Scheme | Monoplane Low wing | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
10.0
88.7
|
|
| Height (m) |
0.6
3.6
50.1
|
|
| Wings | ||
| Wing area (m2) |
1.1
9.7
925
|
|
| Wingspan (Beam) (m) |
0.1
7.8
95
|
|
| Wing loading (kg/m2) |
3.1
338
829
|
|
| Weights | ||
| Empty weight (kg) |
8
2,266
276,800
|
|
| Max. takeoff weight (Gross weight) (kg) |
154
5,706
575,000
|
|
| Loaded weight (kg) |
5
3,266
242,500
|
|
| Capacity | ||
| Crew (per.) |
1
2
112
|
|
| Speeds | ||
| Max. Speed (km/h) |
25
833
28,165
|
at 3048 |
| Сruise Speed (km/h) |
52
628
3,087
|
|
| Power | ||
| Thrust/weight (kN/kg) |
0.0
0.0
2.1
|
|
| Thrust (kN) |
1.5
30
1,914
|
2 powerplants 15 kN each |
| Performance | ||
| Service ceiling (m) |
0.6
12,400
161,544
|
|
| Range (Ferry range) (km) |
4
965
40,700
|
|
| Dynamic Performance | ||
| Rate of climb (m/min) |
1.9
3,660
36,000
|
|
| Stat | ||
| Number built (qt) |
0
2
43,000
|
|
| Introduction | 1962 | |
| First flight | 07.07.1962 | |
