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