SUPER ETENDARD
Specifications | |
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Country of Origin | France |
Builder | DASSAULT-BREGUET |
First flight | May 1958 Etendard IV October 1990 (Upgraded Super Etendard) |
In-service in the French Navy |
1964 Etendard IV June 1993 (Upgraded Super Etendard) |
Similar Aircraft |
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Crew | One |
Role |
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Span | 31 ft, 6 in / 9.60 meters |
Length | 47 ft / 14.31 meters |
Height | 3.85 meters |
Range | 750-1080 nautical miles |
Endurance | 1h45 to 2h15 with réservoir supplémentaire |
Speed |
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Ceiling | 45,000 feet / 13700 meters |
Weight | 11.90 tonnes (6.25 à vide). |
In-Flight Refueling | Yes |
Internal Fuel | 2612 kg |
Payload | 2100 kg w/full int fuel |
Power plant / Thrust | SNECMA 8 K50 jet engine / 5 t |
Armament |
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Systems |
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Special equipment | 6 Oméra 31 cameras (100, 150, 200 and 600 mm) |
Drop Tanks |
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Engine | 1 SNECMA 8K50 @ 5 tonnes thrust |
Sensors | Agave radar, RWR, ballistic bombsight |
User Country |
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Number of units produced | 85 (all types of Super Etendard included) |
French Navy inventory |
52 Super Etendard in two squadrons 5 Etendard IV P |
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