Specifications |
Primary Function | Advanced jet pilot trainer
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Builder | Northrop Corp.
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Power Plant | Two General Electric J85-GE-5 turbojet engines with afterburners
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Thrust | 2,900 pounds (1,315 kilograms) with afterburners
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Length | 46 feet, 4 1/2 inches (14 meters)
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Height | 12 feet, 10 1/2 inches (3.8 meters)
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Wingspan | 25 feet, 3 inches (7.6 meters)
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Speed | 812 mph (Mach 1.08 at sea level)
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Ceiling | Above 55,000 feet (16,667 meters)
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Maximum Takeoff Weight | 12,500 pounds (5,670 kilograms)
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Range | 1,000 miles (870 nautical miles)
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Armament | T-38A: none; AT-38B has provisions for external armament
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Unit Cost | $756,000
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Crew | Two, student and instructor
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Date Deployed | March 1961
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Inventory | Active force, 562; ANG, 0; Reserve 0
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