Editing Dassault Mirage III (section)

===Mirage IIIE===
While the initial Mirage IIIC model was heading towards quantity production, Dassault turned its attention towards the development of a [[multirole fighter|multirole]]/[[air interdiction|strike]] variant of the aircraft.<ref name = "prof 177"/> Efforts in this direction would eventually materialized in the form of the single-seat ''Mirage IIIE''; a two-seat trainer variant of the aircraft was also developed, designated as the ''Mirage IIID''. On 5 April 1961, the first of a batch of three prototypes performed its first flight.<ref name = "prof 177"/>

[[File:Dassault Mirage Cyrano 11 Radar.jpg|thumb|Cutaway view of the Cyrano radar system]]
The Mirage IIIE considerably differed from the earlier Mirage IIIC interceptor. In terms of its airframe, the aircraft possessed a {{convert|300|mm|abbr=on}} forward fuselage extension, which had been made to increase the size of the avionics bay, located directly behind the cockpit. The stretch had also enabled its fuel capacity to be expanded, which had been deemed necessary after several pilots had criticized the Mirage IIIC for having been quite limited in terms of its range.<ref name = "prof 177"/>

Many Mirage IIIEs were fitted with a British-built [[Marconi]] continuous-wave Doppler navigation radar radome on the bottom of the fuselage, underneath the cockpit; in contrast, none of the Mirage IIICs were provided with this apparatus.<ref name = "prof 177"/> A similar inconsistent variation was the presence or absence of a [[high frequency]] (HF) antenna fitted as a forward extension to the vertical tailplane; on some Mirages, the leading edge of the tailplane was a straight line, while on those with the HF antenna the leading edge had a sloping extension forward. The extension appears to have been generally standard on production Mirage IIIAs and Mirage IIICs, but only appeared in some of the Mirage IIIE's export versions. The Mirage IIIE featured Thomson-CSF Cyrano II dual mode air / ground radar; a [[radar warning receiver]] (RWR) system with the antennas mounted in the vertical tailplane; and an Atar 09C engine, the latter being equipped with a petal-style variable exhaust.<ref name = "prof 177"/>

On 14 January 1964, the first production Mirage IIIE was delivered to the AdA, over time, 192 aircraft were eventually delivered to that service. By 1971, this variant had become the most widely exported version of the aircraft.<ref name = "prof 177"/>