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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.
 | A three-view drawing (1653 x 1330) |
| MODEL | Mirage F1C |
| ENGINE | 1 x SNECMA Atar 9K-50, 7200kg of reheat thrust |
| WEIGHTS |
| Take-off weight | 15200 kg | 33510 lb |
| Empty weight | 7400 kg | 16314 lb |
| DIMENSIONS |
| Wingspan | 8.4 m | 27 ft 7 in |
| Length | 15 m | 49 ft 3 in |
| Height | 4.5 m | 14 ft 9 in |
| Wing area | 25 m2 | 269.10 sq ft |
| PERFORMANCE |
| Max. speed | 2350 km/h | 1460 mph |
| Ceiling | 20000 m | 65600 ft |
| Range w/max.payload | 900 km | 559 miles |
| ARMAMENT | 2 x 30mm cannon, 4000kg of weapons |
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