Lockheed U-2

Lockheed U-2
País	E.e.u.u
Papel	Avión de reconocimiento de gran altitud
Primer vuelo	1 de agosto de 1955
Construido	1104

el Lockheed U-2, apodado "Dragon Lady", es un avión de reconocimiento de altitud ultra alta y motor monoplaza estadounidense operado por la Fuerza Aérea de los Estados Unidos (USAF) y previamente volado por la Agencia Central de Inteligencia (CIA). Proporciona día y noche, a gran altitud (70,000 pies; 21,000 m), recopilación de inteligencia para todo tipo de clima. El U-2 también se ha utilizado para la investigación de sensores electrónicos, calibración de satélites, investigación científica y comunicaciones.

Fuente: Lockheed U-2 en Wikipedia

Lockheed P2V-7 (SP-2H) Neptune + Cockpit
Fotógrafo	Cees Hendriks
Localización	Unknow
Fotos	136

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Lockheed U-2S Senior Year Walk Around
Fotógrafo	Vladimir Yakubov
Localización	Capital City Airshow 2016, Sacramento
Fotos	124

Lockheed U-2S Senior Year

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General Characteristics and Role

The Lockheed U-2 Dragon Lady is an American single-jet engine, high-altitude reconnaissance aircraft famous for its role in intelligence gathering during the Cold War. Designed by Lockheed’s Skunk Works under Clarence “Kelly” Johnson, the U-2 was engineered to fly at extreme altitudes—well above 70,000 feet (21,300 meters)—to remain beyond the reach of Soviet interceptors and surface-to-air missiles of the 1950s and early 1960s. The U-2C was an upgraded version of the initial U-2A, featuring a more powerful J75 engine and an enlarged air intake for improved performance. The U-2D was a specialized two-seat trainer variant developed later. The aircraft’s primary role was photographic and signals intelligence (SIGINT) collection deep inside denied airspace, a mission that required the pilot to wear a specialized pressure suit. Its unique high-aspect ratio wings give it glider-like performance, crucial for maintaining altitude and range.

Property	Typical Value (U-2C)
Tipo	High-Altitude, Single-Seat Reconnaissance Aircraft
National Origin	Estados Unidos
Fabricante	Lockheed Skunk Works
Entered Service (U-2A)	1957
Equipo	1 (Pilot) / 2 (Pilot and Instructor/Sensor Operator for U-2D)
Longitud	15.24 m (50 ft 0 in)
Envergadura	24.38 m (80 ft 0 in)
Max Takeoff Weight	Approx. 13,150 kg (28,990 lb)

Powerplant and Performance

Engine (U-2C): 1 x Pratt & Whitney J75-P-13 turbojet engine.
Engine Thrust: Approx. 75.6 kN (17,000 lbf).
Maximum Speed: Approx. 805 km/h (500 mph) / Mach 0.7.
Operational Ceiling: Officially greater than 21,300 m (70,000 ft), earning it the nickname “The Dragon Lady.”
Range: 4,633 km (2,879 miles) on a typical mission.
Sensors: Carried a variety of interchangeable payloads, including specialized large-format cameras (e.g., the A-2) and highly sensitive electronic intelligence (ELINT) and signals intelligence (SIGINT) equipment. The nose and equipment bays are modular.
Landing Characteristics: Due to its extreme wingspan and bicycle-type landing gear, the aircraft is notoriously difficult to land, often requiring a chase car to communicate final speed and altitude to the pilot.

Service History and Legacy

The U-2 Incident: The U-2’s global notoriety began with the 1960 shoot-down of CIA pilot Francis Gary Powers over the Soviet Union while flying a U-2A. This event exposed the highly secret program and dramatically escalated Cold War tensions.
Cuban Missile Crisis: U-2 missions provided definitive photographic evidence of Soviet intermediate-range ballistic missile sites in Cuba in 1962, triggering the Cuban Missile Crisis.
Variants: The U-2 program led to numerous variants, including the U-2R (larger airframe) and the current operational version, the U-2S, which features a modern GE F118 turbofan engine.
The D-Model: The U-2D was primarily used for testing high-altitude sensors and systems, and was also sometimes used for two-seat training.
Longevity: Despite its age and the introduction of advanced satellites and the SR-71 Blackbird, the U-2 remains in service with the US Air Force, having outlasted its supposed successor, the SR-71, due to its operational flexibility and payload capacity.

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