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T-38 Talon

American supersonic jet trainer, active during the Cold War, deployed extensively for NASA astronaut training missions. Key figures: top speed 1,381 km/h, range 1,835 km, service ceiling 15,240 m, max takeoff weight 5,670 kg, built 1,189. In service with 3 air forces as of 2026 — United States (505), Turkey (68), Germany (41).

Northrop T-38 Talon military training aircraft side profile drawing
Side profile · Northrop T-38 Talon · length 14.1 m
Northrop T-38 Talon military training aircraft in flight
Max speed
1,381km/h
Range
1,835km
Produced
1,189units
Active worldwide
614
Technical SpecificationsVersion: T-38A
Crew2
Length14.1 m (46.4 ft)
Wingspan7.7 m (25.3 ft)
Height3.9 m (12.9 ft)
Wing area16 m² (172.2 sqft)
Empty weight3,266 kg (7,200 lbs)
Max. takeoff weight5,670 kg (12,500 lbs)
Powerplant2 × turbojets General Electric J85-GE-5A 1,216 kgf each
Ejection seatMartin-Baker US16T
PerformanceVersion: T-38A
Maximum speed1381 km/h (Mach 1.3)
Operational range1,835 km (1,140 mi)
Service ceiling15,240 m (50,000 ft)
Climb rate170.7 m/s (560.0 ft/s)
Operators — 2026
ActiveOn order
All Operators
🇩🇪 Germany· 🇰🇷 South Korea· 🇵🇹 Portugal· 🇹🇷 Turkey· 🇹🇼 Taiwan· 🇺🇸 United States
Air Bases — 1
🇺🇸 Joint Base Langley–Eustis 71st Fighter Training Squadron
Similar Aircraft
T-38 Talon vs

Description

The T-38 Talon is a twin-engine, high-altitude, supersonic jet trainer used by the United States Air Force (USAF). The program originated in the late 1950s, as the USAF sought a jet trainer to prepare pilots for advanced fighter and bomber aircraft. Developed by Northrop Corporation, now Northrop Grumman, the first T-38 was flown on April 10, 1959. It was introduced into service in 1961 and has been the primary jet trainer for the USAF since then.

Design

The T-38 Talon has a sleek, streamlined design optimized for high-performance flight. It features a tandem-seat cockpit, allowing for a student pilot and an instructor. The aircraft is powered by two afterburning General Electric J85 engines, giving it supersonic capabilities. It has a single-piece canopy for enhanced visibility and a trapezoidal wing shape to reduce drag at high speeds. The T-38's lightweight and simplicity were intentional design choices aimed at reducing operational costs and maintenance requirements.

The T-38 Talon shares a common design lineage with the F-5 Tiger, both being developed based on the Northrop N-156 prototype design. Their airframes are strikingly similar, featuring a twin-engine configuration and a streamlined, aerodynamic shape optimized for high-speed flight. They both employ variants of the General Electric J85 turbojet engine, contributing to their high subsonic and low supersonic performance capabilities. The trapezoidal wing shape is another shared design feature, aimed at reducing drag at high speeds.

Armament

The T-38 Talon is primarily a training aircraft, so it is not heavily armed. The focus of its design is on flight training rather than combat capabilities. That said, some variants have provisions for carrying a limited amount of armaments for training purposes, such as practice bomb dispensers or gun pods. However, these are not standard features and are generally not used during most training sorties. The aircraft's main role is to simulate the flight characteristics of more advanced combat aircraft, so it usually flies unarmed.

Operational History

The T-38 Talon entered service with the United States Air Force in 1961 and quickly became the primary jet trainer. Over 1,100 T-38s have been built, and the aircraft has trained generations of U.S. military pilots. Beyond the USAF, the T-38 is also used by the U.S. Navy, NASA, and several foreign air forces for pilot training.

It has seen various upgrades over its long service life to extend its operational capability, including avionics and structural improvements. While not a combat aircraft, the T-38 has been used in various secondary roles, including target towing and adversary training.

Although several incidents and crashes have occurred over its service history, the T-38 has a generally strong safety record given the number of flight hours accumulated. It is expected to remain in service until at least the 2030s, gradually being replaced by the newer T-7 Red Hawk.

Variants

The T-38 Talon has several variants, including:

  • T-38A: The original production model, used primarily for training.

  • AT-38B: Modified for weapons training, capable of carrying munitions for ground-attack exercises.

  • T-38C: Upgraded version featuring modern avionics and structural improvements for a longer service life.

  • NT-38: A modified version used for various kinds of testing, including NASA experiments.

  • T-38M: Modernized by Turkish Aerospace Industries for the Turkish Air Force, featuring updated avionics and other improvements.

  • QF-38: Converted into target drones for missile testing.

Wikipedia (CC BY-SA) and other open sources. Illustrations generated by AI. Last updated on 23 July 2026. Suggest a change

Frequently Asked Questions

What type of aircraft is the T-38 Talon?
The Northrop T-38 Talon is a military training aircraft aircraft developed by Northrop and entered service in 1961.
What is the maximum speed of the T-38 Talon?
The Northrop T-38 Talon has a maximum speed of 1,381 km/h (Mach 1.3).
What is the range of the T-38 Talon?
The Northrop T-38 Talon has an operational range of 1,835 km (1,140 miles). This range can vary based on payload, altitude, and mission profile.
When did the T-38 Talon first fly?
The Northrop T-38 Talon made its first flight on March 10, 1959. It entered operational service in 1961.
How many T-38 Talon have been built?
Approximately 1,189 units of the Northrop T-38 Talon have been produced since it entered service in 1961.
Which countries operate the T-38 Talon?
The Northrop T-38 Talon is in service with 3 countries, with approximately 614 aircraft in active service. The largest operators include the United States, Turkey, and Germany. 6 countries have operated it in all.
What is the service ceiling of the T-38 Talon?
The Northrop T-38 Talon has a service ceiling of 15,240 meters (50,000 feet). This is the maximum altitude at which the aircraft can maintain controlled flight.
Latest Data Updates
  1. JUL 232026 Updated Sources and cross-references refreshed
  2. APR 72026 Updated Sources and cross-references refreshed
  3. APR 52026 Updated Ejection seat added
  4. JAN 122026 Updated Range updated in a site-wide editorial pass
  5. OCT 222023 Updated Specifications and description reviewed