Skip to content
Vincony — fast, managed web hosting for your next site
The Pilots Desk
modified Lockheed U-2 aircraft used for high-altitude research missions

Lockheed ER-2

Lockheed ER-2

The Lockheed U-2, nicknamed the "Dragon Lady", is an American single-engine, high–altitude reconnaissance aircraft operated by the United States Air Force (USAF) and the Central Intelligence Agency (CIA) since the 1950s. Designed for all-weather, day-and-night intelligence gathering at altitudes above 70,000 feet (21,300 meters), the U-2 has played a pivotal role in aerial surveillance for decades. Lockheed Corporation originally proposed the aircraft in 1953. It was approved in 1954, and its first test flight was in 1955. Between 1956 and 1962, U-2 aircraft conducted covert reconnaissance missions over the Soviet Union, China, Vietnam, and Cuba, gathering critical imagery intelligence throughout the Cold War. In 1960, CIA pilot Gary Powers was shot down in a U-2C over the Soviet Union by a surface-to-air missile (SAM). Major Rudolf Anderson Jr. was shot down in a U-2 during the Cuban Missile Crisis in 1962. U-2s have taken part in post-Cold War conflicts in Afghanistan and Iraq, and supported several multinational NATO operations. Beyond tactical surveillance, U-2s have supported the development of electronic sensors, calibrated space-based instruments, conducted high-altitude atmospheric experiments, and tested line-of-sight and over-horizon communications systems. The U-2 is one of a handful of aircraft types to have served the USAF for over 50 years, along with the Boeing B-52, Boeing KC-135, Lockheed C-130 and Lockheed C-5. The newest models (TR-1, U-2R, U-2S) entered service in the 1980s, and the latest model, the U-2S, had a technical upgrade in 2012. The U-2 is currently operated by the USAF and NASA.

Summary from Wikipedia, photo via Wikimedia Commons, licensed under CC BY-SA.

Country of origin
United States
Length
18.92 m
Wingspan
31.5 m

Specifications

Cruise speed
413 kt
Max speed
70 kt
Range
6,090 nm
Service ceiling
80,000 ft
Rate of climb
9,000 ft/min
Max takeoff weight
40,000 lb
Empty weight
16,000 lb
Fuel capacity
2,950 US gal
Powerplant
General Electric F118-101
Engines
1
Seats
1
Length
63 ft
Wingspan
103 ft
Height
16 ft
Number built
104

Specifications are approximate and may vary by variant. Compiled from Wikipedia (CC BY-SA).

Reference and training only. Specifications vary by variant — consult the manufacturer and the official documents.