| Mirage F2 | |
|---|---|
| Role | Attack fighter |
| National origin | France |
| Manufacturer | Dassault Aviation |
| First flight | 12 June 1966 |
| Number built | 1 |
| Variants | Dassault Mirage G |
The Dassault Mirage F2 was a French prototype two-seat attack fighter which was designed to serve as a test bed for the SNECMA TF306 turbofan engine and influenced the similar variable-geometry Dassault Mirage G.
Dassault were tasked in the early 1960s to design a low-altitude intruder that did not have the high approach speeds associated with the Mirage's delta wing. Unlike the earlier 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 choose 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]
Data from [1]Illustrated Encyclopedia of Aircraft
General characteristics
Performance
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