Mirage F2 / F3

In the early 1960s, Dassault was tasked with designing a low-altitude intruder to address the high approach speeds associated with the delta wing design of the Mirage III. Unlike the Mirage III, the F2 featured a high-mounted swept wing and horizontal tail surfaces. Initially powered by a Pratt & Whitney TF30 turbofan, the prototype achieved its first flight on June 12, 1966. Subsequently, it was re-engined with the SNECMA TF306 for its second flight on December 29, 1966.

While two parallel developments explored a single-seat Mirage F3 interceptor and a scaled-down Mirage F1, the French Air Force ultimately chose to develop the French-engined F1, leading to the discontinuation of the F2 program. The F2's fuselage and engine served as the foundation for a variable-geometry variant, the Mirage G.

Being a prototype aircraft, the Dassault Mirage F2 did not see operational deployment. Its primary role was as a test bed for the SNECMA TF306 turbofan engine and to explore design concepts for a low-altitude intruder, and it never entered production or active service.

Main Variants:

• Mirage F3: A single-seat interceptor variant explored in parallel development.

• Mirage F1: A scaled-down version selected for production by the French Air Force.

• Mirage G: A variable-geometry variant developed from the F2's fuselage and engine.