Dassault Mirage F1 playing 'Star Wars' in Chad
The
Dassault Mirage F1 is a
French single-seat air-superiority fighter and attack aircraft designed and built by
Dassault Aviation as a successor of the
Mirage III family.
The Mirage F1 entered service in the
French Air Force in the early seventies. Powered by a single
SNECMA Atar turbojet providing about 7 tonnes of thrust, the F1 has been used as a light multipurpose fighter and has been exported to about a dozen nations. More than 700 F1s have been produced.[1]. Among the second generation
European supersonic fighter (ie, among those built in the sixties and early seventies) the F1 was the most successful, most significantly because almost all of its users have used it in wars and regional conflicts.
Due to the success of the
Mirage F1 in the export market, the airplane has seen combat with a number of air forces in various places around the world.
France
French Air Force
Mirage F1s saw their first operational deployment in
1984 during
Operation Manta, the
French intervention in the
Chad, to counter growing
Libyan encroachment. Four Mirage F1C-200s provided air cover for a force of four Jaguars, and took part in skirmishes against the pro-Libyan
GUNT rebels.
In
1986, French Mirage F1s returned to Chad, as part of
Operation Epervier, with four F1C-200s providing fighter cover for a strike package of eight Jaguars during the air raid against the Libyan airbase at Ouadi Doum, on
February 16. Two F1CRs also flew pre and post-strike reconnaissance missions.[14][15]
More recently, in
October 2007, three Mirage
2000s and three Mirage F1s have been deployed at
Kandahar Air Force Base, where they fly close air support and tactical reconnaissance missions in support of international forces in
Southern Afghanistan.
Specifications (Mirage F1)
Orthographically projected diagram of the Dassault Mirage F1
General characteristics
*
Crew: 1
*
Length: 15.33 m (50 ft 3 in)
*
Wingspan: 8
.44 m (27 ft 8 in)
*
Height: 4.49 m (14 ft 8 in)
*
Wing area: 25 m² (270 ft²)
*
Empty weight: 7,400 kg (16,
000 lb)
*
Loaded weight: 11,130 kg (24,540 lb)
*
Max takeoff weight: 16,
200 kg (35,700 lb)
*
Powerplant: 1× SNECMA Atar 9K-50 afterburning turbojet
Performance
*
Maximum speed:
Mach 2.
3 (2,573 km/h, 1,600 mph) at 11,000 m (36,000 ft)
*
Combat radius: 425 km (229 nm, 265 mi)
*
Ferry range: 2,
150 km (1,160 nm, 1,335 mi)
*
Service ceiling: 20,000 m (66,000 ft)
*
Rate of climb: 215 m/s (42,
300 ft/min)
*
Wing loading: 450 kg/m² (91 lb/ft²)
*
Thrust/weight: 0.64
Armament
*
Guns: 2×
30 mm (1.18 in)
DEFA 553 cannons with 150 rounds per gun
*
Rockets: 8×
Matra rocket pods with 18×
SNEB 68 mm rockets each
*
Missiles: 4×
AIM-9 Sidewinders OR Matra R550 Magics, 2×
Super 530Fs, 2×
AM-39 Exocets, 2×
AS-30L
*
Bombs: 14,000 lb (6,300 kg) of payload on five external hardpoints, including a variety of bombs, reconnaissance pods or
Drop tanks