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Lockheed T-1 SeaStar (T2V SeaStar) Naval Jet Trainer


Like the T-33, the T-1 SeaStar was born from the success of the Lockheed F-80 Shooting Star jet platform.

 Updated: 5/21/2012; Authored By Staff Writer; Content ¬©www.MilitaryFactory.com

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Lockheed T2V-1 SeaStar Technical Specifications



Service Year: 1957
Type: Naval Jet Trainer
National Origin: United States
Manufacturer(s): Lockheed - USA
Production Total: 150


Structural (Crew Space, Dimensions and Weights)



Operating Crew (Typical): 2
Overall Length: 38.55 feet (11.75 meters)
Overall Width: 42.85 feet (13.06 meters)
Overall Height: 13.32 feet (4.06 meters)

Weight (Empty): 11,964 lb (5,427 kg)
Weight (MTOW): 16,834 lb (7,636 kg)

Installed Power and Standard Day Performance



Propulsion: 1 x Allison J33-A-24/24A turbojet developing 6,100lbs of thrust.

Maximum Speed: 580 mph (933 kph; 504 knots)
Maximum Range: 969 miles (1,560 km)
Service Ceiling: 39,993 feet (12,190 meters; 7.57 miles)
Rate-of-Climb: 6,330 feet-per-minute (1,929 m/min)

Armament / Mission Payload



None.

Global Operators / Customers



United States

Model Variants (Including Prototypes)



L-245 - Lockheed Model Designation
T2V-1 - Original US Navy Designation prior to 1962.
T-1A SeaStar - US Navy Designation after 1962.