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Mirage IV  
Initial Operational Capability (IOC): 1964
Total Production: 62
Also Known As: Mirage IVA and Mirage IVP
Origin: France
Corporations: Dassault-Aviation
Parent System: Mirage III
Initial Operational Capability (IOC): 1961
Total Production: ?
Family Members: Mirage III
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Description: Dassault Mirage IV was a twin-engine, two-seat, supersonic, nuclear attack aircraft derived from Mirage III tactical fighter. It featured a delta-wing and was powered by two Snecma Atar 9K engines rated at 15,875 pounds of thrust each with afterburning. In its nuclear deterrence role, Mirage IV was equipped with an ASMP nuclear-capable supersonic cruise missile. The French Air Force ordered 62 aircraft with the first one achieving Initial Operational Capability in 1964. In the 1990s and 2000s Mirage IVP were used to conduct reconnaissance flights. The last Mirage IV, a IVP model, arrived at the French Air Museum on June 30, 2005. From 1964 through 2005, Mirage IVs logged 337,000 flight hours.

Mirage IV Specifications

Crew: 2
Number of Engines: 2
Height: 5.65 meter (18.5 foot)
Length: 23.5 meter (77 foot)
Wingspan: 11.9 meter (38.9 foot)
Ceiling: 20,000 meter (65,617 foot)
Max Range: 2,480 kilometer (1,339 nautical mile)
Top Speed at High Altitude: 649 mps (2,337 kph)
Empty Weight: 14,500 kilogram (31,966 pound)
Max Takeoff Thrust: 31,750 pound (14,402 kilogram)
Max Takeoff Weight: 31,600 kilogram (69,665 pound)
Payload: 7,200 kilogram (15,873 pound)
CEP: Circular Error Probable
Meters (m)   Kilometers (km)   Nautic Miles (nm)   Inch (in)   Yard (yd)   Foot (ft)   Millimeter (mm)
Pound (lb)   Kilogram (kg)   kN (KiloNewton)   Ton (t)
Meters per Second (mps)   Kilometers per Hour (kph)   Knot (kt)   Miles per Hour (mph)
Liter (l)   Galon (gl)
Year (yr)   Minutes (min)   Second (sec)
Shaft-Horse-Power (shp)

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