AMD Mirage F-1CG


Manufacturer:
Dassault Aviation (previously Avions Marcel Dassault- Breguet Aviation) 
Country of origin:
France
Specification:Mirage F1CG
Type:
fighter
Crew:
Pilot on a Martin Baker Mk 6 zero/zero ejection seat.
Entry into service:1975
Withdrawn:
2003
Armaments:
Two 30 mm DEFA 553 cannon with 135 rounds per gun in the underside of the forward fuselage.Up to 8,818 lb (4000 kg) of disposable stores carried on seven hardpoints (one under the fuselage rated at 4,630 lb/2100 kg, four under the wings with the inner two units each rated at 2,866 lb/1300 kg and the outer two units each at 1,213 lb/550 kg, and two at the wing tips with each unit rated at 331 lb/150 kg); the two wing tip hardpoints can each carry one AIM-9J/P Sidewindwer.Greek Mirage F-1s have the outer wimg hardpoinds modified to carry Sidewinders  too. 
Electronics & equipment:
Standard communication and navigation equipment, plus  Thomson-CSF Cyrano IV radar.
Powerplant:One SNECMA Atar 9K-50 turbojet rated at 11,023lb st (49.03 kN) dry and 15,785 lb st (70.21 kN) with afterburning.
Fuel capacity:
Internal fuel 1,135.9 US gal (945.9 Imp gal; 4300 liters); external fuel up to one 581.2 US gal (483.9 Imp gal; 2200 liter) and two 298.5 US gal (248.6 Imp gal; 1130 liter) drop tanks; no provision for inflight refueling.
Dimensions:
Span 27 ft 6.75 in (8.40 m) without tip stores and about 30 ft 6.75 in (9.32 m) with tip-mounted  AAMs; aspect ratio 2.82; area 269.11sq ft (25.00 m2).
Length 50 ft 2.5 in (15.30 m); height 14 ft 9 in (4.50 m); wheel track 8 ft 2.5 in (2.50 m); wheel base 16 ft 4.75 in (5.00 m).
Operational weights:Empty 16,314 lb (7400 kg); normal take-off 24,030 lb (10900 kg); maximum take-off 35,715 lb (16200 kg).
Maximum speed:
Maximum level speed 'clean' 1,262 kt (1,453 mph; 2338 km/h) or Mach 2.20 at 36,090 ft (11000 m).
Maximum range:
749 nm (863 miles; 1390 km),approx. endurance 2 hours 15 minutes on a CAP with two  AAMs and one drop tank.
Performance:
Maximum rate of climb at sea level 41,930 ft (12780 m) per minute with afterburning; service ceiling 65,615 ft (20000 m).