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| U. S.
Military Aircraft Lockheed T2V-1 SEASTAR Photo By Coll B. Thouanel |
|
At the beginning of the 1950s the US Navy's standard advanced trainer was the TV-2, the naval version of the T-33A land based trainer. Though it was an effective trainer the TV-2 was not ideally suited to the navy's requirements as it lacked carrier compatibility. Lockheed had already proposed its L-245 design for an improved version of the T-33, and confident that this would prove successful, built a private venture prototype. This was known unofficially as the T-33B and first flew in December 1953. The prototype introduced a raised instructor's seat under a revised canopy, and a flight trials revealed the need for a dorsal fin to restore longitudinal stability. Other changes were leading edge slats, a larger tail unit, and a boundary layer control system. This resulted in take off and approach speed being usefully reduced. The navy ordered the type as the T2V-1 Seastar with an arrester hook, non jettison able tip tanks, a strengthened airframe, and beefed up land gear. The first of 150 Seastar entered service 1n 1957, and in 1962 the type was redesigned T-1A. The type's service career was short because of maintenance problems. |
TECHNICAL DATA
| Description | Specifications |
| Manufacturer: Lockheed | Length: 38 ft. 6.5 in. |
| First Flight: December 1953 | Height: 13 ft. 4 in. |
| Model: T2V-1 | Wing Span: 42 ft. 10 in. |
| Crew: Two | Wing Area: 240.0 sq. ft. |
| Nickname: Seastar | Empty Weight: 11,965 lb. |
| Basic Role: Trainer | Max. Weight: 16,800 lb. |
| Other Versions: T2V-1 sole production model. | Armament: None |
| Principal User: |
Propulsion |
|
USA. Performance |
Power Plant: Allison J33-A-24A turbojet. |
| Range: 970 miles | Horsepower: 6,100-lb thrust |
| Max. Speed: 580 mph. | No. Of Engines: One |
| Ceiling: 40,000 ft. | |
| Climb Rate: 6,330 ft. per minute. |