The Dassault Mirage F2 was a French prototype two-seat ground attack/fighter aircraft, which was designed to serve as a test bed for the SNECMA TF306 turbofan engine. The F2 also influenced the subsequent Dassault Mirage G, a variable geometry design.

Dassault were tasked in the early 1960s to design a low-altitude intruder that did not have the high approach speeds associated with the delta wing of the Mirage III. Unlike the Mirage III, the F2 had a high-mounted swept wing and horizontal tail surfaces. The prototype powered by a Pratt & Whitney TF30 turbofan first flew on 12 June 1966. It was re-engined with the SNECMA TF306 for the second flight on 29 December 1966.

Two parallel developments were a single-seat Mirage F3 interceptor and a scaled-down and simpler Mirage F1. Eventually the French Air Force chose to develop the French-engined F1, and the F2 did not enter production.^[1]

The fuselage and engine from the F2 formed the basis of a variable-geometry variant, the Mirage G.^[1]

The Mirage F2 is now preserved with DGA Techniques Aeronautiques in Toulouse Balma.^{[citation needed]}

Data from the Illustrated Encyclopedia of Aircraft.^[1]

General characteristics

• Crew: 2
• Length: 17.60 m (57 ft 9 in)
• Wingspan: 10.50 m (34 ft 5 in)
• Height: 5.80 m (19 ft 0 in)
• Empty weight: 9,500 kg (20,944 lb)
• Max takeoff weight: 18,000 kg (39,683 lb)
• Powerplant: 1 × Pratt & Whitney TF30 turbofan, 89 kN (20,000 lbf) thrust

Performance

• Maximum speed: 2,333 km/h (1,450 mph, 1,260 kn)
• Maximum speed: Mach 2.2
• Service ceiling: 20,000 m (66,000 ft)

Related development

• Dassault Mirage III
• Dassault Mirage F1
• Dassault Mirage G