SUPER ETENDARD
| Specifications | |
|---|---|
| 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 |
|
| Crew | One |
| Role |
|
| 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 |
|
| 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 |
|
| Systems |
|
| Special equipment | 6 Oméra 31 cameras (100, 150, 200 and 600 mm) |
| Drop Tanks |
|
| 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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