Dassault Mirage F1
1966
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Dassault Mirage F1

Evolved in parallel with the Mirage F2 as a scale-down, multi-role single-seat fighter employing a SNECMA Atar turbojet, the Mirage F1 was conceived as a successor to the Mirage IIIC and was the subject of a government contract awarded in 1964. Possessing, like the F2, a conventional sweptback wing generously equipped with high-lift devices, and conventional swept tail surfaces, the private venture prototype F1 flew on 23 December 1966. Three pre-series aircraft were ordered in September 1967, the first of these flying on 20 March 1969. The initial production model for France's Armee de l'Air was designated F1C, placed emphasis on the intercept mission, was powered by an Atar 9K-50 turbojet affording 7200kg with afterburning, and had an armament of two 30mm cannon, two Matra 550 Magic and two Matra R 530 or Super 530 AAMs. An initial order for the F1C for the Armee de l'Air was placed in 1969, 162 being procured by that service (plus 64 recce F1CRs and 20 two-seat F1B trainers), initial operational capability being achieved in 1974. Many of the Armee de l'Air aircraft were delivered in, or retroactively modified to, F1C-200 standard with a 8cm fuselage plug to accommodate a removable flight refuelling probe. Variants of the basic aircraft offered for export, in addition to the F1C, were the F1A with simplified avionics for operation under VFR conditions and the F1E multi-role air superiority/ground attack/reconnaissance version. Export customers were Ecuador (16 F1AJs), Greece (40 F1CGs), Iraq (113 F1EQs), Jordan (17 F1CJs and 17 F1EJs), Kuwait (27 F1CKS), Libya (16 F1ADs and 16 F1EDs), Morocco (30 F1CHs and 20 F1EHs), Qatar (12 F1EDAs), South Africa (32 F1AZs and 16 F1CZs) and Spain (45 F1CEs and 22 F1EEs). Production of the Mirage F1 was completed in 1990 with 731 built (including F1B and F1D two-seat trainers and F1CR reconnaissance aircraft). In 1991, work began on the adaptation of 30 F1C-200S as F1CT ground attack fighters.

3-View 
Dassault Mirage F1A three-view drawing (1653 x 1330)


Specification 
 MODELMirage F1C
 ENGINE1 x SNECMA Atar 9K-50, 7200kg of reheat thrust
 WEIGHTS
    Take-off weight15200 kg33510 lb
    Empty weight7400 kg16314 lb
 DIMENSIONS
    Wingspan8.4 m27 ft 7 in
    Length15 m49 ft 3 in
    Height4.5 m14 ft 9 in
    Wing area25 m2269.10 sq ft
 PERFORMANCE
    Max. speed2350 km/h1460 mph
    Ceiling20000 m65600 ft
    Range w/max.payload900 km559 miles
 ARMAMENT2 x 30mm cannon, 4000kg of weapons

Dassault Mirage F1

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