Dassault Mirage F2

Dassault Aviation · France · first flew 1966 · fighter

The Dassault Mirage F2 was a French prototype two-seat ground attack and fighter aircraft. It was designed as a test bed for the SNECMA TF306 turbofan engine.

Recognition (WEFT)

W — WingsHigh-mounted, swept
E — Engines1 × turbofan, fuselage-mounted
F — Fuselage17.6 m fuselage
T — TailConventional

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Unlike the Mirage III it has a high-mounted swept wing and horizontal tail surfaces. It is a single-engined two-seater.

Specifications

Figures are for the representative variant described above; marks differ. See how AircraftIQ sources figures.

History

Dassault was tasked in the early 1960s with designing a low-altitude intruder without the high approach speeds of the Mirage III delta wing. The prototype, powered by a Pratt & Whitney TF30 turbofan, first flew on 12 June 1966.

Variants

Two parallel developments were the single-seat Mirage F3 interceptor and the scaled-down Mirage F1. The F2 fuselage and engine formed the basis of the variable-geometry Mirage G.

Where you'll see it

The Mirage F2 did not enter production, as the French Air Force chose to develop the French-engined F1. It was re-engined with the SNECMA TF306 for its second flight on 29 December 1966.

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