T-38 Talon
U.S. Air Force Photo by TSgt Fernando Serna
The instructor and student sit in tandem on rocket-powered ejection seats in a pressurized, air-conditioned cockpit. Critical components are waist high and can be easily reached by maintenance crews. Refueling and preflight inspections are easily performed.
The T-38 needs as little as 2,300 feet (695.2 meters) of runway to take off and can climb from sea level to nearly 30,000 feet (9,068 meters) in one minute.
Test pilots and flight test engineers are trained in T-38A's at the U.S. Air Force Test Pilot School at Edwards Air Force Base, Calif. Air Force Materiel Command uses T-38A's to test experimental equipment such as electrical and weapon systems.
Pilots from most North Atlantic Treaty Organization countries are trained in the T-38A at Sheppard AFB, Texas, through the Euro-NATO Joint Jet Pilot Training Program.
The National Aeronautics and Space Administration uses T-38A aircraft as trainers for astronauts and as observers and chase planes on programs such as the space shuttle.
Air Education and Training Command uses a modified version, the AT-38B, to prepare pilots for fighter aircraft such as the F-15, F-16 and A-10. and F-111. This model carries external armament and weapons delivery equipment for training.
The Talon first flew in 1959. More than 1,100 were delivered to the Air Force between 1961 and 1972 when production ended. Approximately 562 remain in service throughout the Air Force.
An ongoing program called Pacer Classic, the structural life extension program for the T-38, is integrating 10 modifications, including major structural renewal, into one process. As a result, the service life of T-38s should extend to the 2010. Additionally, the introduction of the T-1A Jayhawk significantly relieved the T-38's work load.
Builder: Northrop Corp.
Power Plant: Two General Electric J85-GE-5 turbojet engines with afterburners
Thrust: 2,900 pounds (1,315 kilograms) with afterburners
Length: 46 feet, 4 1/2 inches (14 meters)
Height: 12 feet, 10 1/2 inches (3.8 meters)
Wingspan: 25 feet, 3 inches (7.6 meters)
Speed: 812 mph (Mach 1.08 at sea level)
Ceiling: Above 55,000 feet (16,667 meters)
Maximum Takeoff Weight: 12,500 pounds (5,670 kilograms)
Range: 1,000 miles (870 nautical miles)
Armament: T-38A: none; AT-38B has provisions for external armament
Unit Cost: $756,000
Crew: Two, student and instructor
Date Deployed: March 1961
Inventory: Active force, 562; ANG, 0; Reserve 0
keywords: aircraft, training