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Dassault Mirage Milan (Kite)


Single-Seat, Single-Engine Strike Fighter Prototype (1970)


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The Dassault Milan, with its unique retractable foreplane arrangement, was unsuccessfully proposed to the Swiss Air Force as a strike solution.



Authored By: Staff Writer | Last Edited: 05/28/2019 | Content ©www.MilitaryFactory.com | The following text is exclusive to this site.
It only seemed natural to continue the successful line of supersonic single-seat, single-engine jet-powered fighters by Dassault of France down various roads. The Cold War-era delta-winged platform, begun with the "Mirage III" model of 1961, this entry going on to see total serial production reach 1,422 units with military operators all over the globe - the French Air Force becoming the largest with 348 units accepted. The success of Mirage III has been embodied by the facst that the series continues to fly today (2019) with the Pakistan Air Force as 89 are committed to the service. Other notable Mirage family fighter forms became the "Mirage IIIV", "Mirage 5", and South African Atlas "Cheetah" - all detailed elsewhere on this site.

It was inevitable that this same aircraft family continued to be branched across efforts intended to produce an even better end-product for either local or global customers. Such was the case with the Mirage "Milan" that was proposed in the latter part of the 1960s as a single-seat, single-engine strike-minded aircraft. The design, developed through a joint-venture with the Swiss-based company "Fabrique Federale d'Avions" ("Swiss Federal Aircraft Factory" = SFAF), produced several flyable prototypes to prove the aircraft sound - a first-flight recorded on September 27th, 1968. At this point in history, the Swiss Air Force was in the running to succeed its aging stock of British-borne Hawker "Hunter" jet-powered fighters.

The key change to the Mirage III design was the implementation of retractable, forward-cranked foreplanes regarded as "moustaches". These were situated along the sides of the forward fuselage section and used to improve controlling of the aircraft at low-level, low-speed flight envelopes - mainly during take-off, landing, and attack actions. The first base development airframe was an existing Mirage 5J No.2 aircraft and this was then joined by a modified Mirage IIIR model. In time, the aircraft came to be known as the "Milan" ("Kite") and a definitive, third, prototype entry converted from a Mirage IIIE joined the development phase.

The relatively simply modification to the existing, proven Mirage III design led to an aircraft having greater Maximum Take-Off Weight (MTOW) capabilities which resulted in greater war loads over range. Additionally, take-off runs were shortened and low-altitude handling was improved as expected. On the whole, the main form (single-engine, single-rudder fin, side-mounted intakes, tricycle undercarriage, etc...) and function of the aircraft were retained which meant that all of the strengths of the original design were still apparent throughout the Milan. Early testing with the moustache foreplanes was conducted on a Mirage platform with fixed versions of the wings, this phase completed in March of 1969.

The Mirage IIIE prototype, "Milan S-01", finished with reworked avionics and powered by a single SNECMA "Atar" 9K50 afterburning turbojet engine of 15,885lb thrust output (the changes intended to better mimic the production-quality form), took to the air for the first time on May 29th, 1970.

The production version of the aircraft was to be recognized as the "Milan S" and carry the navigation-attack system already fitted (and proven) in the SEPECAT "Jaguar" strike aircraft line. The Milan was slated for initial deliveries to expecting customers in 1972.

As completed, the strike fighter featured a standard armament fit of 2 x 30mm ADEN automatic cannons with an optional war load rated up to 8,800lb, all in the form of externally-held ordnance. Ordnance options were to include the usual gamut of conventional drop bombs of various potency, air-to-surface rocket pods, and jettisonable fuel stores (the latter to increase operational ranges). Weapons were mounted to seven hardpoints found under the aircraft include a fuselage centerline location and three under-root, underwing positions at each side.

The capable Milan was offered to the Swiss Air Force alongside the America-originated LTV A-7 "Corsair II" - a capable strike fighter in its own right - but the service eventually elected to continue operating its fleet of Hawker Hunters for the time being - leaving the Mirage Milan to the pages of military aviation history.

Specifications



Service Year
1970

Origin
France national flag graphic
France

Status
CANCELLED
Development Ended.
Crew
1

Production
3
UNITS


Dassault Aviation - France
National flag of Switzerland Switzerland (rejected)
(OPERATORS list includes past, present, and future operators when applicable)
Ground Attack (Bombing, Strafing)
Ability to conduct aerial bombing of ground targets by way of (but not limited to) guns, bombs, missiles, rockets, and the like.
Close-Air Support (CAS)
Developed to operate in close proximity to active ground elements by way of a broad array of air-to-ground ordnance and munitions options.
Intelligence-Surveillance-Reconnaissance (ISR), Scout
Surveil ground targets / target areas to assess environmental threat levels, enemy strength, or enemy movement.
X-Plane (Developmental, Prototype, Technology Demonstrator)
Aircraft developed for the role of prototyping, technology demonstration, or research / data collection.


Length
49.4 ft
(15.05 m)
Width/Span
27.1 ft
(8.25 m)
Height
14.8 ft
(4.50 m)
Empty Wgt
16,535 lb
(7,500 kg)
MTOW
33,069 lb
(15,000 kg)
Wgt Diff
+16,535 lb
(+7,500 kg)
(Showcased structural values pertain to the Dassault S-01 (Prototype) production variant)
Installed: 1 x SNECMA Atar 9K-50 afterburning turbojet engine developing 15,885lb of thrust.
Max Speed
1,491 mph
(2,400 kph | 1,296 kts)
Ceiling
54,134 ft
(16,500 m | 10 mi)
Range
2,082 mi
(3,350 km | 6,204 nm)
Rate-of-Climb
16,500 ft/min
(5,029 m/min)


♦ MACH Regime (Sonic)
Sub
Trans
Super
Hyper
HiHyper
ReEntry
RANGES (MPH) Subsonic: <614mph | Transonic: 614-921 | Supersonic: 921-3836 | Hypersonic: 3836-7673 | Hi-Hypersonic: 7673-19180 | Reentry: >19030


(Showcased performance specifications pertain to the Dassault S-01 (Prototype) production variant. Compare this aircraft entry against any other in our database. View aircraft by powerplant type)
PROPOSED, STANDARD:
2 x 30mm ADEN automatic cannons mounted internally.

PROPOSED, OPTIONAL:
Up to 8,818lb of externally-held stores across seven hardpoints to include conventional drop bombs, rocket pods, and jettisonable fuel tanks.


Supported Types


Graphical image of an aircraft automatic cannon
Graphical image of aircraft aerial rockets
Graphical image of an aircraft rocket pod
Graphical image of an aircraft conventional drop bomb munition
Graphical image of an aircraft external fuel tank


(Not all ordnance types may be represented in the showcase above)
Hardpoint Mountings: 7


Milan ("Kite") - Base Project Designation.
Milan S-01 - Initial prototype from the Mirage IIIE framework.
Milan S - Proposed production-quality versions designation.


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