| Type | Aircraft | |
| Company | Lockheed Corporation | |
| Scheme | High wing Monoplane | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
16.3
88.7
|
|
| Height (m) |
0.6
6.9
50.1
|
|
| Wings | ||
| Wing area (m2) |
1.1
55.6
925
|
|
| Wingspan (Beam) (m) |
0.1
9
95
|
Folded |
|
0.1
20.9
95
|
Unfolded | |
| Weights | ||
| Empty weight (kg) |
8
12,056.9
276,800
|
|
| Max. takeoff weight (Gross weight) (kg) |
154
23,831.3
575,000
|
|
| Capacity | ||
| Crew (per.) |
1
4
112
|
Pilot, Co-Pilot/COTAC, TACCO, Sensor Operator/TFO |
| Speeds | ||
| Ground Speed (km/h) |
96.6
795
1,500
|
at sea level |
| Max. Speed (km/h) |
25
828
28,165
|
at 6100 m |
| Сruise Speed (km/h) |
52
649
3,087
|
|
| Fuel | ||
| Fuel Capacity (l) |
23
7,191.3
320,000
|
Internal fuel capacity |
| Fuel External (l) |
142.5
2,272
10,025
|
2x 1,136 L tanks |
| Power | ||
| Thrust/weight (kN/kg) |
0.0
0.4
2.1
|
|
| Thrust (kN) |
1.5
82.5
1,914
|
2 powerplants 41,26 kN each |
| Performance | ||
| Service ceiling (m) |
0.6
12,466.3
161,544
|
|
| Range (Ferry range) (km) |
4
5,120.8
40,700
|
|
| Сombat radius (km) |
277
853
7,210
|
|
| Endurance (h) |
0.0
7.3
150
|
|
| Dynamic Performance | ||
| Rate of climb (m/min) |
1.9
1,560.6
36,000
|
|
| Combat | ||
| Bombs weight (kg) |
2
2,220
39,000
|
on four internal and two external hardpoints |
| Stat | ||
| Number built (qt) |
0
188
43,000
|
|
| Price (USD) |
41.5
27.0 million
750.0 million
|
|
| Introduction | 1974 | |
| First flight | 21.01.1972 | |
