French prototype jet fighter
The Dassault Étendard VI was a French prototype fighter aircraft initially developed as part of the NATO NBMR-1 competition to find a standard fighter to serve amongst member air forces. Dassault took advantage of the fact that the French Air Force had issued a requirement around the same time for a new fighter-bomber and developed aircraft in parallel as variations of the same design concept for the two prospective customers.
Originally designated Mystère XXVI, the aircraft was accepted as one of the entrants to be developed to prototype stage for a fly-off with competing designs. It fared well in test flights, but was out-performed by the Aeritalia G.91 that was eventually selected as the winner of the competition.
A further development of the Étendard concept, the Étendard IV was successfully developed for French Navy service.
Specifications
Data from [citation needed]
General characteristics
- Crew: 1
- Length: 10.85 m (35 ft 7 in)
- Wingspan: 8.3 m (27 ft 3 in)
- Height: 3.76 m (12 ft 4 in)
- Wing area: 23 m2 (250 sq ft)
- Empty weight: 3,720 kg (8,201 lb)
- Max takeoff weight: 5,860 kg (12,919 lb)
- Powerplant: 1 × Bristol Siddeley Orpheus turbojet, 21.6 kN (4,900 lbf) thrust
Performance
- Maximum speed: 912 km/h (567 mph, 492 kn)
- Range: 890 km (550 mi, 480 nmi)
- Service ceiling: 13,400 m (44,000 ft)
- Wing loading: 255 kg/m2 (52 lb/sq ft)
- Thrust/weight: 0.38
Armament
- Guns: ** 2× 30 mm (1.18 in) cannons or
- Bombs: 1,000 kg (2,200 lb) of bombs and rockets
See also
Related development
Aircraft of comparable role, configuration, and era
Related lists
References
Bibliography
- Carbonel, Jean-Christophe (2016). French Secret Projects. Vol. 1: Post War Fighters. Manchester, UK: Crecy Publishing. ISBN 978-1-91080-900-6.
