| Type | Aircraft | |
| Company | Lockheed Corporation | |
| Scheme | Integrated Monoplane | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
31.0
88.7
|
|
| Height (m) |
0.6
5.6
50.1
|
|
| Wings | ||
| Wing area (m2) |
1.1
141.1
925
|
|
| Wingspan (Beam) (m) |
0.1
17.0
95
|
|
| Weights | ||
| Empty weight (kg) |
8
24,800
276,800
|
|
| Capacity | ||
| Crew (per.) |
1
1
112
|
2 for trainer variant |
| Payload (kg) |
23
1,100
122,470
|
of reconnaissance sensors |
| Speeds | ||
| Max. Speed (km/h) |
25
3,560
28,165
|
at 23000 |
| Сruise Speed (km/h) |
52
2,125
3,087
|
|
| Fuel | ||
| Fuel Capacity (l) |
23
46,180
320,000
|
|
| Power | ||
| Thrust/weight (kN/kg) |
0.0
0.6
2.1
|
|
| Thrust (kN) |
1.5
288
1,914
|
2 powerplants 144 kN each |
| Performance | ||
| Service ceiling (m) |
0.6
29,000
161,544
|
|
| Range (Ferry range) (km) |
4
4,000
40,700
|
|
| Dynamic Performance | ||
| Rate of climb (m/min) |
1.9
36,000
36,000
|
|
| Stat | ||
| Number built (qt) |
0
12
43,000
|
|
| Introduction | 1962 | |
| First flight | 26.04.1962 | |
| Stop production | 1968 | |
