Rafale C
Rafale B
Rafale M
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Data for: Rafale C
Manufacturer: | Avions.Marcel.Dassault-Breguet.Aviation,.France | Max.speed: | 2.070.km/h | (1.286 mph) | Length: |
Type: | multirole fighter aircraft | Comb..range: | 1.852 km | (1.150 mi) | Span: |
Description: | built as Jaguar and Super Etendard replacement | Range: | 3.700+ km | (3.000+ mi) | Height: |
First flight: | 1986 | Ceiling: | 16.800 m | (55.000 ft) | Max.weight: |
Crew: | 1 | Climb rate: | 304,8 m/s | (60.000.ft/min) | Numb. built: |
15,27 m | (50 ft 1 in) |
10,80 m | (35 ft 5 in) |
5,34 m | (17 ft 6 in) |
24.500 kg | (54.013 lb) |
93 (Rafale | total, Dec.2010) |
Engines: | 2 x SNECMA M88-2 turbofans | ||
Thrust: | 2 x 50,04 kN (2 x 11.250 lbf) dry thrust | ||
2 x 75,62 kN (2 x 17.000 lbf) with afterburner | |||
Armament: | Gun: 1 x 30 mm (1 x 1.18 in) | ||
Hardpoints: 14 | |||
Hardpoints capacity: 9.500 kg (21.000 lb) |
More info/sources: |
Wikipedia |
Aviastar |
Dassault |
Global Aircraft |
Air Attack |
Data for: Rafale B
Manufacturer: | Dassault Aviation, France | Max speed: | 2.070 km/h | (1.286 mph) | Length: |
Type: | fighter-trainer | Combat range: | 1.852 km | (1.150 mi) | Span: |
Description: | Rafale trainer version | Range: | 3.700+ km | (3.000+ mi) | Height: |
First flight: | 1993 | Ceiling: | 16.800 m | (55.000 ft) | Max.weight: |
Crew: | 2 | Climb rate: | 304,8 m/s | (60.000 ft/min) | Numb. built: |
15,27 m | (50 ft 1 in) |
10,80 m | (35 ft 5 in) |
5,34 m | (17 ft 6 in) |
24.500 kg | (54.013 lb) |
38 (2011) |
Engines: | 2 x SNECMA M88-2 turbofans | ||
Thrust: | 2 x 50,04 kN (2 x 11.250 lbf) dry thrust | ||
2 x 75,62 kN (2 x 17.000 lbf) with afterburner | |||
Armament: | Gun: 1 x 30 mm (1 x 1.18 in) | ||
Hardpoints: 14 | |||
Hardpoints capacity: 9.500 kg (21.000 lb) |
More info/sources: |
Wikipedia |
Aviastar |
Dassault |
Airwar |
Data for: Rafale M
Manufacturer: | Dassault Aviation, France | Max speed: | 2.070 km/h | (1.286 mph) | Length: |
Type: | naval fighter | Comb. range: | 1.760 km | (1.095 mi) | Span: |
Description: | navalised Rafale with strengthened structure | Range: | 2.000 km | (1.245 mi) | Height: |
and landing gear and with longer nose gear | Ceiling: | 16.765 m | (55.005 ft) | Max weight: | |
First flight: | 1991 | Climb rate: | 330 m/s | (64.960 ft/min) | Numb. built: |
Crew: | 1 |
15,27 m | (50 ft 1 in) |
10,80 m | (35 ft 5 in) |
5,34 m | (17 ft 6 in) |
22.500 kg | (49.605 lb) |
31 (2011) | |
Engines: | 2 x SNECMA M88-2 turbofans | ||
Thrust: | 2 x 50,04 kN (2 x 11.250 lbf) dry thrust | ||
2 x 75,62 kN (2 x 17.000 lbf) with afterburner | |||
Armament: | Gun: 1 x 30 mm (1 x 1.18 in) | ||
Hardpoints: 13 | |||
Hardpoints capacity: 9.500 kg (21.000 lb) |
More info/sources: |
Airwar |
Wikipedia |
Dassault |
French Fleet Air Arm |
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