Dassault Étendard IV

Length
14.35 m
Flat Wing Span
9.6 m
Height
3.9 m
Flat Wing Area
28.4 m²
Max Speed
1099 km/h
Max Ceiling
15500 m
Number of Engines
1
First Flight
1956-07-24
Entry Into service
1962-01-01
Number Built
90
Maximum Take-Off Weight
10.2 t (paragliders: kg)
Maximum Range
3300 km

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Aircraft Weight Variants

Aircraft Maximum Take-Off Weight (t (paragliders: kg)) Maximum Range (km)
Dassault Étendard IV 10.2 3300

Similar airplanes

All data (24 fields)
Name
Dassault Étendard IV
Manufacturer
Dassault Aviation
Description
The Dassault Étendard IV is a transonic carrier-borne strike fighter aircraft developed and manufactured by French aerospace company Dassault Aviation.
First Flight
1956-07-24
Entry Into service
1962-01-01
Service End
1991-01-01
Designer
Dassault Aviation
Type
Strike fighter
Length (m)
14.35
Height (m)
3.9
Cockpit Crew
1
Max Speed (km/h)
1099
Max Ceiling (m)
15500
Rate of Climb (m/s)
100
Armament
2 × 30 mm (1.18 in) DEFA 552 cannons with 150 rounds per gun; 1,360 kg (3,000 lb) of payload on four external hardpoints, including a variety of bombs or Drop tanks; 2 × Matra rocket pods with 18× SNEB 68 mm rockets each; AIM-9 Sidewinder and Matra Magic air-to-air missiles, Nord AS.30 and AS.20 air-to-surface missiles.
National Origin
France
Number Built
90
Powerplant Description
1 × SNECMA ATAR 08B turbojet engine, 43.16 kN thrust each
Primary Users
French Navy
Status
Retired
Wikipedia Article (URL)
en.wikipedia.org/wiki/Dassault_%C3%89tendard_IV
Flat Wing Span (m)
9.6
Flat Wing Area (m²)
28.4
Number of Engines
1