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U-2S Dragon Lady

U-2S Dragon Lady

Surveillance & Reconnaissance Airplanes
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Basic Information
Name
U-2S Dragon Lady
Designation
U-2S Dragon Lady
Alternate Designation
Block 10 U-2, Block 20 U-2, ER-2, TR-1A, TR-1B, U-2A, U-2B, U-2C, U-2D, U-2R, U-2RT
Equipment Type
Surveillance & Reconnaissance Airplanes
Manufacturer
Lockheed Martin
Date of Introduction
1994
Description

The U-2S provides continuous day and night, high altitude, all weather, surveillance of an area in support of US forces. It provides intelligence to decision makers through all phases of conflict, including peacetime indications and warnings, crises, operations other than war and major theater war. The U-2S Dragon Lady is a single seat, single engine, reliable, high altitude reconnaissance aircraft. Due to high altitude flight the pilot must wear a full pressure suit. It carries a variety of sensors such as film photo, Synthetic Aperture Radar, or Electro-Optical devices and features a high mission success rate. The information collected during its mission can be relayed to control stations via line-of-sight and beyond-line-of-sight (via satellite) data-links. The first U-2 model made its maiden flight in 1995. In 1962 an U-2 photographed the Soviet missiles being installed on Cuban territory. It provided critical intelligence data during operation Desert Storm in 1991, and Allied Force in 1999. Before operation Iraqi Freedom in 2003 the U-2S were involved in reconnaissance flights over Iraq searching for potential weapons of mass destruction sites. In the late 1990s despite Global Hawk ISR UAV availability, the US Air Force was upgrading the U-2S Dragon Lady to extend its service life through 2020. The modernization program was expected to be completed by 2007. Following QDR 2006 the US Air Force plans for the U-2 aircraft were to complete its retirement by fiscal year 2011. Due to year 2012 US Air Defense budget cuts the U-2S retirement date was delayed to 2040. In February 2014, the Pentagon due to budget cuts decided to put an end to the U-2 program.

Air & Air Defense Specifications
Crew 1
Max Speed 694.8 km/h
Range 9700.0 km
Service Ceiling 21350 m
Wingspan 31.40 m
Overview (Deagel)
Group Surveillance & Reconnaissance Airplanes
Status Active
Also Known As Block 10 U-2, Block 20 U-2, ER-2, TR-1A, TR-1B, U-2A, U-2B, U-2C, U-2D, U-2R, U-2RT
Origin United States of America
Contractor Lockheed Martin
Initial Operational Capability (IOC) 1994
Total Production 35
Specifications (Deagel)
Crew 1
Number of Engines 1
Dimensions — Height 4.9 meter
Dimensions — Length 19.2 meter
Dimensions — Wingspan 31.4 meter
Mass — Empty Weight 7,260 kilogram
Mass — Max Takeoff Thrust 17,000 pound
Mass — Max Takeoff Weight 18,150 kilogram
Performance — Ceiling 21,350 meter
Performance — Max Range 9,700 kilometer
Speed — Top Speed at High Altitude 193 mps
Time — Flight Endurance 10 hour
Gear (Deagel)
Item 1 ESM & Warning Systems: AN/ASQ-230 ASIP (1)
Item 2 Fighter Aircraft Engines: F118-GE-101 (1)
Item 3 Jamming Systems: AN/ALQ-196
Item 4 Jamming Systems: AN/ALQ-221 ADS (1)
Item 5 Mapping Systems: ASARS-2 (1)
Item 6 Mapping Systems: ASARS-2B (1)
Details
Country of Origin United States
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
19.2 m
Width
31.4 m
Height
4.9 m
Weight
18150 kg
Operators (1)
United States
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