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Encyclopedia > Dassault Etendard II
Dassault Etendard II
Description
Role Fighter-bomber
Crew One, pilot
First Flight July 23, 1956
Manufacturer Dassault
Dimensions
Length 12.89 m 41 ft 3 in
Wingspan 8.74 m 27 ft 11 in
Height 3.80 m 12 ft 2 in
Wing area 24.2 m² 248 ft²
Weights
Empty 4,210 kg 9,260 lb
Loaded
Maximum takeoff 5,650 kg 12,430 lb
Powerplant
Engines 2x Turbomeca Gabizo
Thrust 18.4 kN 4,136 lb
Performance
Maximum speed 1,054 km/h 659 mph
Range 1,100 km 688 miles
Service ceiling 15,000 m 48,000 ft
Rate of climb
Wing loading 233 kg/m² 50 lb/ft²
Thrust/Weight 3.3 N/kg 0.33 lbf/lb
Avionics
Avionics
Armament
Guns 2x 30 mm cannons
Stores 1,500 kg (3,300 lb) of bombs and rockets

The Dassault Etendard II was a French prototype fighter aircraft initially developed as a follow-on project to the Dassault Mystère series. It was presented to the French Air Force for evaluation but was rejected in favour of the Dassault Mirage III.


Originally designated Mystère XXII, the aircraft was developed in response to a French Air Force requirement for a light, jet-powered fighter-bomber. At around the same time, a NATO requirement was circulated, also calling for a light strike-fighter, and Dassault developed a very similar aircraft in parallel for that competition (the Etendard VI).


The sole prototype of the Etendard II flew on July 23, 1956 but proved to be somewhat underpowered and showed nothing like the promise of the Mirage series and was quickly abandoned.


A further development of the Etendard concept, the Etendard IV was successfully developed for French Navy service.

Related content
Related Development Etendard IV - Etendard VI - Super Etendard
Similar Aircraft
Related Lists List of military aircraft of France - List of fighter aircraft

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  Results from FactBites:
 
Dassault Etendard II - strike fighter (234 words)
Dassault prepared a basic design to meet both requirements, and, being of the opinion that the officially-backed specifications would result in underpowered aircraft, evolved a third version of the design as a private venture.
The three versions of the aircraft were designated Etendard (Standard) II, IV and VI, and the first to commence its flight test programme was the Etendard II.
Competing with the Breguet 1100, the Etendard II was powered by two 940kg Turbomeca Gabizo turbojets and proposed armament included two 30mm cannon which were to be installed as a pack interchangeable with one containing 32 Matra 105 68mm rockets.
HHQ - DB2000 Encyclopedia (184 words)
Dassault developed the Etendard to meet a NATO requirement for a light strike fighter.
The requirement for an Etendard replacement was to originally be met by a navalised development of the SEPECAT Jaguar.
This failed to eventuate and the French navy eventually settled on Dassaults proposal for the Super Etendard.
  More results at FactBites »

 

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