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Designed to replace Lockheed T-33, F-5A flew on July 30, 1959.
Entered production in October 1963.
T-38 "Talon" with two seats flew on April 10, 1959.
| CREW | 1-2 |
| ENGINE | 2 x General Electric J-85-GE-13, 18.1kN |
| WEIGHTS |
| Take-off weight | 9117 kg | 20100 lb |
| Empty weight | 3565 kg | 7860 lb |
| DIMENSIONS |
| Wingspan | 7.7 m | 25 ft 3 in |
| Length | 14.4 m | 47 ft 3 in |
| Height | 4.0 m | 13 ft 1 in |
| Wing area | 15.8 m2 | 170.07 sq ft |
| PERFORMANCE |
| Max. speed | M1.4 | M1.4 |
| Ceiling | 16000 m | 52500 ft |
| Range w/max.payload | 592 km | 368 miles |
| ARMAMENT | 2 x 20mm machine-guns |
| jeelocked, white-mailbox(@)netzero.com, 01.04.2008 See "Northrop T-38 Talon" (next in list) for comments on company funded devrelopement and dev history... |
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