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Description
| Manufacturer: | Lockheed | |
| Base model: | U-2 | |
| Designation: | WU-2 | |
| Version: | A | |
| Designation System: | U.S. Air Force | |
| Designation Period: | 1952-Present | |
| Basic role: | Utility | |
| Modified Mission: | Weather reconnaissance | |
Specifications
| Length: | 49' 7" | 15.1 m | |
| Height: | 13' | 3.9 m | |
| Wingspan: | 80' | 24.3 m | |
| Empty Weight: | 11,700 lb | 5,306 kg | |
| Gross Weight: | 15,850 lb | 7,188 kg | |
| Max Weight: | 21,000 lb | 9,523 kg | |
Propulsion
| No. of Engines: | 1 | ||
| Powerplant: | Pratt & Whitney J75-P-37A | ||
| Thrust (each): | 11,000 lb | 4,988 kg | |
Performance
| Range: | 2,200 miles | 3,542 km | |
| Cruise Speed: | 460 mph | 740 km/h | 400 kt |
| Max Speed: | 494 mph | 795 km/h | 429 kt |
| Ceiling: | 55,000 ft | 16,763 m | |
