Mirage F2 / F3

🇫🇷France
Dassault
1966 – Present
Overview
Mirage F2 / F3
The Dassault Mirage F2, designed in the early 1960s as a low-altitude intruder, featured a high-mounted swept wing and was initially powered by a Pratt & Whitney TF30 turbofan before being re-engined with the SNECMA TF306. Although it served as a prototype and test bed for engine and design concepts, it was ultimately discontinued in favor of the Mirage F1, with no operational deployment or production.
Specifications

General

Crew1
Max Speed Mach1.34 Mach
Service Ceiling M20,000 m
Research Notes

Swept-wing alternative to the Mirage delta formula

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The Mirage F2/F3 effort grew from French requirements for a low-altitude, all-weather aircraft with better short-runway behavior than pure delta-wing Mirages. Dassault replaced the delta with a high swept wing and conventional tail, using the program to explore a different aerodynamic path.

Prototype focused on low-altitude attack and interception

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The two-seat Mirage F2 was intended as a low-altitude intruder and fighter concept, while the related F3 was a single-seat interceptor direction. The design demonstrated useful ideas, but it competed with simpler and more affordable paths that led toward the Mirage F1.

No operational service but clear design influence

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The Mirage F2/F3 did not enter production, so its importance is developmental. It informed later Dassault work, including variable-geometry studies, and helps explain why the Mirage F1 departed from the company's earlier delta-wing pattern.

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