High Gallery
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U. S.
Military Aircraft U-2 (TR-1A) Photo Coll B. Thouanel |
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The U-2 multi sensor reconnaissance and surveillance plane first flew in Article 341 prototype form during August 1955, and was followed by a comparatively small number of production aircraft stretching from the original U-2A to the current TR-1. The type was capable of extended cruise at so high an altitude that it was thought invulnerable to Soviet air defenses until a U-2B was down over the USSR by a Soviet surface to air missile in May 1960. The aircraft of the U-2 series, especially the initial machine, were very tricky to fly, and after the loss of several single seat it was thought essential to develop a two seat conversion trainer. At least two such trainer were produced by converting one U-2C and one U-2D into U-2CTs with the instructor's cockpit locate behind and above the standard cockpit using the volume of the erstwhile Q-bay, where the inertial navigation system and other electronic were previously accommodated. |
| Lockheed U-2CT |
TECHNICAL DATA
| Description | Specifications |
| Manufacturer: Lockheed | Length: 50 ft. 0 in. |
| First Flight: August 1955 | Height: 15 ft. 0 in. |
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Model:U-2CT |
Wing Span: 80 ft. 0 in. |
| Crew: Two | Wing Area: 565.0 sq. ft. |
| Nickname: | Empty Weight: |
| Basic Role: Trainer | Max. Weight: 22,542 lb. |
| Other Versions: U-2CT sole trainer model. | Armament: None. |
| Principal User: USA. |
Propulsion |
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Performance |
Power Plant: Pratt & Whitney J57-P-13B. |
| Range: 2,880 miles. | Horsepower: 17,000-lb thrust. |
| Max. Speed: 460 mph. | No. Of Engines: |
| Ceiling: 70,000 ft. | One |
| Climb Rate: |