Lockheed Corporation
Lockheed U-2S
The Lockheed U‑2S is the most recent variant of the legendary high‑altitude reconnaissance aircraft originally conceived by Lockheed Corporation in the mid‑1950s. The program began when the CIA sought a platform capable of flying above 70,000 feet to capture photographic intelligence over hostile territory, leading to the first flight in August 1955 and operational service in 1956. Over six decades the airframe has been continuously upgraded; the U‑2S, introduced in 2010, incorporates a modernized Pratt & Whitney F118‑101 turbofan, digital avionics, and an advanced sensor suite that includes electro‑optical, infrared and synthetic‑aperture radar payloads. Its 103‑foot wings and lightweight aluminum‑titanium structure provide the lift‑to‑drag ratio needed for sustained flight at the edge of the stratosphere, while a pressurized cockpit and autonomous flight‑control system reduce pilot workload. The U‑2S remains a critical element of U.S. and allied intelligence, having supplied decisive imagery during the Cold War, the Gulf conflicts, and contemporary operations against emerging threats. Its longevity demonstrates the unique value of ultra‑high‑altitude platforms in an era dominated by satellites and unmanned aircraft. Its proven reliability and low operational cost make it a versatile asset for both strategic surveillance and scientific research missions, ensuring its relevance well into the next decade.
Classification
Dimensions
- Length
- 19.2 metre
- Height
- 5.09 metre
- Mass
- 18144 kilogram
Performance
- Maximum Speed
- 356 knot
- Service Ceiling
- 21336 metre
- Range
- 11265 kilometre
Production & History
- Units Produced
- 31
Design & Classification
- Country of Origin
- Manufacturer
- Lockheed Corporation
- Engine
- General Electric F118
- Operator
-
United States Air Force
- Wikidata ID
- Q112151026