In numbers Through the lens Video
Three-view drawing
Technical specifications
|
DESIGNER
|
Avions Marcel Dassault |
|---|---|
|
COUNTRY
|
France |
|
TYPE
|
Multipurpose fighter |
|
CREW
|
1 |
|
POWER-PLANT
|
One Snecma Atar 9K-50 turbojet engine |
| Thrust, kgf | 1x7.200 |
|
DIMENSIONS
|
|
|
Length, m
|
15,20 |
|
Height, m
|
4,50 |
|
Wing span, m
|
9,32 |
|
Wing area m2
|
25,00 |
| WEIGHT | |
| Maximum take-off, kg | 16.200 |
| Normal take-off, kg | - |
| Empty aircraft, kg | 7.400 |
| Internal fuel, kg | - |
| Warload, kg | 4.000 |
| PERFORMANCE | |
| Maximum permitted speed at high altitude, km/h (11.000 m), km/h | 2.720 |
| Maximum speed in low height, km/h | 1.470 |
|
Maximum overload, g
|
-
|
|
Rate of climb, m/min
|
12.600
|
| Service ceiling, m | 18.500 until 20.000 |
| Range, km | 3.300 |
| Combat range, km | 800 |
| ARMAMENT | Two 30 mm cannons DEFA 553 with 2x135 rounds. Number external hardpoints: 7. Transportation of weapons: air-to-air missiles Matra 550 Magic, Matra Super 530 (medium range). Air-to-surface missile AS.30, AS.30L or AS-37 Martel. 400, 250, 125 kg or 1.000 kg or ΒΑΡ-100 (ΒΑΡ-120 bomb against self-propelled targets). Dassault CC421 30 mm DEFA. Rocket launcher of 18 or 36 missiles. ster bombs BLG66 Belouga or 12x BAP-100. or 2 pods Dattack CC421 with 30-mm cannon DEFA. |
Photos Mirage F1CG
Dassault-Breguet Mirage F-1CG Museum of History (Athens, HAF)
