|
 |
|
|
 |
| |
T38
Specifications |
|
| |
Primary
Function |
Advanced jet
pilot trainer |
|
| |
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 |
|
| |
Crew |
Two, student and
instructor |
|
| |
Date Deployed |
March 1961 |
|
 |
|
|
 |