In numbers Through the lens Video
The plane remained active up to her beginning of decade ' 90 (with final ' withdrawn in 1993).
Technical specifications
|
DESIGNER
|
Locheed Martin |
|---|---|
|
COUNTRY
|
USA |
|
TYPE
|
Training aircraft |
|
CREW
|
2 |
|
POWER-PLANT
|
One General Electric J79-GE-11A turbojet engine |
| Thrust, kgf | 1x7.070 |
|
DIMENSIONS
|
|
|
Length, m
|
16,69 |
|
Height, m
|
4,11 |
|
Wing span (not including wing tip fuel tanks), m
|
6,68 |
|
Wing area m2
|
18,22 |
| WEIGHT | |
| Maximum take-off, kg | 13.170 |
| Normal take-off, kg | 9.000 |
| Empty aircraft, kg | 6.350 |
| Internal fuel, kg | 2.650 |
| Warload, kg | 1.814 |
|
PERFORMANCE
|
|
|
Maximum speed, km/h
|
2.214 |
| Maximum speed in low height, km/h | 1.473 |
|
Maximum overload, g
|
-
|
|
Rate of climb, m/min
|
-
|
| Service ceiling, m | 18.300 |
|
Ferry range, km
|
3.510
|
| Range, km | 1.740 |
| Combat range, km | - |
| ARMAMENT | One six-barrel cannon General Electric M61A1 Vulcan with 725 rounds. Number external hardpoints: 5 (plus two Sidewinder missiles on the wings tips). Possibility of transport air-to-air missile AIM-9L Sidewinder, air-to-surface missile AGM-12B. Air guided bombs. Free falling bombs. |
Photos ΤF-104G Starfighter
