Mirage IV
Mirage IV
Attack Aircrafts
Basic Information
Name
Mirage IV
Designation
Mirage IV
Alternate Designation
Mirage IVA, Mirage IVP
Equipment Type
Attack Aircrafts
Manufacturer
Dassault-Aviation
Date of Introduction
1964
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.
Air & Air Defense Specifications
Crew
2
Max Speed
2336.4 km/h
Range
2480.0 km
Service Ceiling
20000 m
Wingspan
11.90 m
Overview (Deagel)
Group
Attack Aircrafts
Status
Retired - No Longer Operational
Also Known As
Mirage IVA, Mirage IVP
Origin
France
Contractor
Dassault-Aviation
Initial Operational Capability (IOC)
1964
Total Production
62
Specifications (Deagel)
Crew
2
Number of Engines
2
Dimensions — Height
5.7 meter
Dimensions — Length
23.5 meter
Dimensions — Wingspan
11.9 meter
Mass — Empty Weight
14,500 kilogram
Mass — Max Takeoff Thrust
31,750 pound
Mass — Max Takeoff Weight
31,600 kilogram
Mass — Payload
7,200 kilogram
Performance — Ceiling
20,000 meter
Performance — Max Range
2,480 kilometer
Speed — Top Speed at High Altitude
649 mps
Gear (Deagel)
Item 1
Cruise Missiles: ASMP (1)
Variants
Variant 1
Mirage III
Variant 2
Mirage IV
Details
Country of Origin
France
Sources
deagel.com: https://www.deagel.com/x/x/a000733
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
23.5 m
Width
11.9 m
Height
5.7 m
Weight
31600 kg
Operators (1)
France
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