The
Mirage III is a supersonic fighter aircraft designed in France
by Dassault Aviation during the late 1950s,
and manufactured both in France and a number of other
countries. It was a successful
fighter aircraft, being sold to many
air forces around the world and remaining
in production for over a decade. Some of the world's smaller air
forces still fly Mirage IIIs or variants as front-line equipment
today.
Development
The Mirage III family grew out of French government studies begun
in 1952 that led in early 1953 to a specification for a
lightweight, all-weather
interceptor capable of climbing to
18,000 m (59,040 ft) in six minutes and able to reach
Mach 1.3 in level flight.
Dassault's response to the specification was the
Mystère-Delta 550, a diminutive and
sleek jet that was to be powered by twin
Armstrong Siddeley MD30R Viper
afterburning
turbojets, each with thrust of
9.61 kN (2,160 lb
f). A SEPR liquid-fuel
rocket motor was to provide additional burst
thrust of 14.7 kN (3,300 lb
f). The aircraft had a
tailless
delta configuration, with a 5%
chord (ratio of airfoil thickness to length) and 60 degree
sweep.
The tailless delta configuration has a number of limitations. The
lack of a
horizontal
stabilizer meant
flaps cannot be
used, resulting in a long takeoff run and a high landing speed. The
delta wing itself limits maneuverability; and suffers from
buffeting at low altitude, due to the large wing area and resulting
low
wing loading. However, the delta is
a simple and pleasing design, easily built and robust, capable of
high speed in a straight line, and with plenty of space in the wing
for fuel storage.
The first prototype of the Mystere-Delta, without afterburning
engine or rocket motor and with an unusually large vertical
tailfin, flew on 25 June 1955. After some redesign, reduction of
the tailfin to more rational size, installation of afterburners and
rocket motor, and renaming to
Mirage I, in late
1955, the prototype attained Mach 1.3 in level flight without
rocket assist, and Mach 1.6 with the rocket.
However, the small size of the Mirage I restricted its armament to
a single
air-to-air missile, and
even before this time it had been prudently decided the aircraft
was simply too tiny to carry a useful warload. After trials, the
Mirage I prototype was eventually scrapped.
Dassault then considered a somewhat bigger version, the
Mirage II, with a pair of
Turbomeca Gabizo turbojets, but no aircraft
of this configuration was ever built. The Mirage II was bypassed
for a much more ambitious design that was 30% heavier than the
Mirage I and was powered by the new
SNECMA
Atar afterburning turbojet with thrust of 43.2 kN (9,700
lb
f).
The Atar was an axial flow turbojet, derived
from the German
World War II BMW 003
design.
The new fighter design was named the
Mirage III.
It incorporated the new
area ruling
concept, where changes to the cross section of an aircraft were
made as gradual as possible, resulting in the famous "wasp waist"
configuration of many supersonic fighters. Like the Mirage I, the
Mirage III had provision for a SEPR rocket engine.

Cutaway view of the Cyrano radar
system
The prototype Mirage III flew on 17 November 1956, and attained a
speed of Mach 1.52 on its seventh flight. The prototype was then
fitted with the SEPR rocket engine and with manually-operated
intake half-cone shock diffusers, known as
souris
("mice"), which were moved forward as speed increased to reduce
inlet turbulence. The Mirage III attained a speed of Mach 1.8 in
September 1957.
The success of the Mirage III prototype resulted in an order for 10
preproduction
Mirage IIIAs. These were almost two
meters longer than the Mirage III prototype, had a wing with 17.3%
more area, a chord reduced to 4.5%, and an Atar 09B turbojet with
afterburning thrust of 58.9 kN (13,230 lb
f). The SEPR
rocket engine was retained, and the aircraft were fitted with
Thomson-CSF Cyrano Ibis air intercept radar, operational avionics,
and a drag chute to shorten landing roll.
The first Mirage IIIA flew in May 1958, and eventually was clocked
at Mach 2.2, making it the first European aircraft to exceed Mach 2
in level flight. The tenth IIIA was rolled out in December 1959.
One was fitted with a
Rolls-Royce
Avon 67 engine with thrust of 71.1 kN (16,000 lb
f)
as a test model for
Australian evaluation,
with the name "Mirage IIIO". This variant flew in February 1961,
but the Avon powerplant was not adopted.

The belly of a Mirage III
Mirage IIIC and Mirage IIIB
The first major production model of the Mirage series, the
Mirage IIIC, first flew in October 1960. The IIIC
was largely similar to the IIIA, though a little under a half meter
longer and brought up to full operational fit. The IIIC was a
single-seat interceptor, with an Atar 09B turbojet engine,
featuring an "eyelet" style variable exhaust.
The Mirage IIIC was armed with twin 30 mm
DEFA revolver-type cannon, fitted in the belly
with the gun ports under the air intake. Early Mirage IIIC
production had three stores pylons, one under the fuselage and one
under each wing, but another outboard pylon was quickly added to
each wing, for a total of five. The outboard pylon was intended to
carry a
Sidewinder air-to-air missile (AAM), later replaced
by
Matra Magic.
Although provision for the rocket engine was retained, by this time
the day of the high-altitude bomber seemed to be over, and the SEPR
rocket engine was rarely or never fitted in practice. In the first
place, it required removal of the aircraft's cannon, and in the
second, apparently it had a reputation for setting the aircraft on
fire. The space for the rocket engine was used for additional fuel,
and the rocket nozzle was replaced by a ventral fin at first, and
an airfield arresting hook assembly later.
A total of 95 Mirage IIICs were obtained by the
AdA, with initial operational deliveries in
July 1961. The Mirage IIIC remained in service with the AdA until
1988.
The French
Armée de l'Air (AdA)
also ordered a two-seat
Mirage IIIB operational
trainer, which first flew in October 1959. The fuselage was
stretched about a meter (3 ft 3.5 in) and both cannons were removed
to accommodate the second seat. The IIIB had no radar, and
provision for the SEPR rocket was deleted, although it could carry
external stores. The AdA ordered 63 Mirage IIIBs (including the
prototype), including five
Mirage IIIB-1 trials
aircraft, ten
Mirage IIIB-2(RV) inflight refueling trainers with dummy
nose probes, used for training
Mirage
IVA bomber pilots, and 20
Mirage IIIBEs, with
the engine and some other features of the multi-role Mirage IIIE.
One Mirage IIIB was fitted with a
fly-by-wire flight control system in the
mid-1970s and redesignated
Mirage IIIB-SV
(
Stabilité Variable); this aircraft was used as a testbed
for the system in the later
Mirage
2000.
Mirage IIIE
While the Mirage IIIC was being put into production, Dassault was
also considering a multi-role/strike variant of the aircraft, which
eventually materialized as the
Mirage IIIE. The
first of three prototypes flew on 1 April 1961.
The Mirage IIIE differed from the IIIC interceptor most obviously
in having a 300 mm (11.8 in) forward fuselage extension to increase
the size of the avionics bay behind the cockpit. The stretch also
helped increase fuel capacity, as the Mirage IIIC had marginal
range and improvements were needed. The stretch was small and hard
to notice, but the clue is that the bottom edge of the canopy on a
Mirage IIIE ends directly above the top lip of the air intake,
while on the IIIC it ends visibly back of the lip.
Many Mirage IIIE variants were also fitted with a Marconi
continuous-wave Doppler navigation radar radome on the bottom of
the fuselage, under the cockpit. However, while no IIICs had this
feature, it was not universal on all variants of the IIIE. A
similar inconsistent variation in Mirage fighter versions was the
presence or absence of an
HF antenna
that was 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 export versions of the Mirage
IIIE.
The 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, with a
petal-style variable exhaust.
The first production Mirage IIIE was delivered to the
AdA in January 1964, and a total of 192
were eventually delivered to that service.
Total production of the Mirage IIIE, including exports, was
substantially larger than that of the Mirage IIIC, including
exports, totaling 523 aircraft. In the mid-1960s one Mirage IIIE
was fitted with the improved SNECMA Atar 09K-6 turbojet for trials,
and given the confusing designation of
Mirage
IIIC2.

Nose of a Mirage IIIR: thinner than
the fighter version, this nose has several glass apertures for
medium-format cameras.
Mirage IIIR
A number of reconnaissance variants were built under the general
designation of
Mirage IIIR. These aircraft had a
Mirage IIIE airframe; Mirage IIIC avionics; a camera nose and
unsurprisingly no radar; and retained the twin DEFA cannon and
external stores capability. The camera nose accommodated up to five
OMERA cameras.
The AdA obtained 50 production Mirage IIIRs, not including two
prototypes. The Mirage IIIR preceded the Mirage IIIE in operational
introduction. The AdA also obtained 20 improved
Mirage
IIIRD reconnaissance variants, essentially a Mirage IIIR
with an extra panoramic camera in the most forward nose position,
and the Doppler radar and other avionics from the Mirage
IIIE.
Exports and license production
Exports
The
largest export customers for Mirage IIICs built in France were
Israel
and South Africa
as the Mirage IIICZ. Some
export customers obtained the Mirage IIIB, with designations only
changed to provide a country code.
Such as the Mirage IIIDA
for Argentina
, Mirage IIIDBR and Mirage
IIIDBR-2 for Brazil
.
Mirage IIIBJ for Israel
,
Mirage IIIDL for Lebanon
,
Mirage IIIDP for Pakistan
,
Mirage IIIBZ and Mirage IIIDZ and
Mirage IIID2Z for South
Africa, Mirage IIIDE for Spain
and
Mirage IIIDV for Venezuela
.
After the
outstanding Israeli success with the Mirage IIIC, scoring kills
against Syrian
Mikoyan-Gurevich MiG-17s and
MiG-21 aircraft and then
achieving a formidable victory against Egypt
, Jordan
, and
Syria
in the Six-Day War of
June 1967, the Mirage III's reputation was greatly enhanced.
The "combat-proven" image and low cost made it a popular export
success.
A good
number of IIIEs were built for export as well, being purchased in
small quantities by Argentina
as the Mirage IIIEA and
Mirage IIIEBR-2 Brazil
as the
Mirage IIIEBR, Lebanon
as the
Mirage IIIEL, Pakistan
as the
Mirage IIIEP, South
Africa as the Mirage IIIEZ, Spain
as the
Mirage IIIEE, and Venezuela
as the Mirage IIIEV, with a list
of subvariant designations, with minor variations in equipment
fit. Dassault believed the customer was always right, and
was happy to accommodate changes in equipment fit as customer needs
and budget required. Pakistani
Mirage 5PA3, for
example, were fitted with Thomson-CSF Agave radar with capability
of guiding the
Exocet anti-ship missile.
Some customers obtained the two-seat Mirage IIIBE under the general
designation
Mirage IIID, though the trainers were
generally similar to the Mirage IIIBE except for minor changes in
equipment fit. In some cases they
were identical, since
two surplus AdA Mirage IIIBEs were sold to Brazil under the
designation
Mirage IIIBBR, and three were
similarly sold to Egypt under the designation
Mirage
5SDD.
New-build exports of this type included
aircraft sold to Abu
Dhabi
, Argentina, Brazil, Chile
, Colombia
, Egypt
, Gabon
, Libya
, Pakistan,
Peru
, Spain, Venezuela, and Zaire
.
Export
versions of the Mirage IIIR were built for Pakistan
as the
Mirage IIIRP and South
Africa as the Mirage IIIRZ, and Mirage
IIIR2Z with an Atar 9K-50 jet engine. Export
versions of the IIIR recce aircraft were purchased by Abu Dhabi,
Belgium, Colombia, Egypt, Libya, Pakistan, and South Africa. Some
export Mirage IIIRDs were fitted with British Vinten cameras, not
OMERA cameras. Most of the Belgian aircraft were built
locally.
License production
The Mirage IIIE was also built under license in Australia, Belgium
and Switzerland.
Australia
While an
experimental Rolls-Royce
Avon-powered version did not enter production, the Australian
government decided that the Royal Australian Air Force (RAAF)
would receive the IIIE, albeit a variant assembled by the Government Aircraft Factory
(GAF) in Fishermans Bend,
Melbourne
from Australian-made components, under the
designation Mirage IIIO. The major
difference between the IIIE and the IIIO was the avionics
installed. The other major Australian aircraft manufacturer at the
time, the
Commonwealth
Aircraft Corporation (CAC), also in Melbourne, built the SNECMA
Atar engine.
GAF produced two variants: the
Mirage IIIO(F),
which was an interceptor, and the Mirage
IIIO(A),
a surface attack aircraft. Dassault produced two sample IIIO(F)
aircraft, with the first flying in March 1963. GAF completed 48
IIIO(F) and 50 IIIO(A) aircraft.
All the surviving Mirage IIIO(F) aircraft were converted to IIIO(A)
standard between 1967 and 1979. The Mirage was finally withdrawn
from RAAF service in 1988, and 50 surviving examples were sold to
Pakistan in 1990.
Belgium
Switzerland
The
Mirage IIIC was built in Switzerland
by F+W Emmen (to day RUAG) (the
federal government aircraft factory in Emmen
) as the Mirage IIICS. As in
Australia, one French-made aircraft was bought in preparation for
license construction. Cost overruns during the production led to
the so-called
"Mirage
affair". In all, 36 Mirage IIIS interceptors, with strengthened
wings, airframe, and
undercarriage.
The Swiss air force required performances comparable to those of
embarked carrier planes.
Avionics differed
as well, with the most prominent difference being that the
Thomson-CSF Cyrano II radar was replaced by Hughes TARAN-18 system,
giving the Mirage IIIS compatibility with the Hughes
AIM-4 Falcon AAM.
In the early 1990s, the 30 surviving Swiss Mirage IIIS interceptors
were put through an upgrade program, which included fitting them
with fixed canards and updated avionics.
Switzerland also only bought a Mirage IIIR variant, designated
Mirage IIIRS, as a prelude to license manufacture,
and built 17 more. Like the Mirage IIIS, Switzerland's Mirage IIIRS
aircraft were later upgraded to feature fixed canards and new
avionics.
Derivatives
Mirage 5/Mirage 50
The next major variant, the
Mirage 5, grew out of
a request to Dassault from the
Israeli
Air Force. The first Mirage 5 flew on
19
May 1967. It looked much like the Mirage
III, except it had a long slender nose that extended the aircraft's
length by about half a metre.The Mirage 5 itself led directly to
the Israeli
Nesher, either through a
Mossad (Israeli intelligence) intelligence
operation or through covert cooperation with
AdA (Armée de l'Air — the French Air
Force), depending upon which story is accepted. (See details in the
Nesher article.) In either case, the design gave
rise to the
Kfir, which can be considered a
direct descendant of the
Mirage III.
Milan
In 1968, Dassault, in cooperation with the Swiss, began work on a
Mirage update known as the
Milan ("
Kite"). The main feature of the Milan was a pair
of pop-out foreplanes in the nose, which were referred to as
"moustaches". The moustaches were intended to provide better
take-off performance and low-speed control for the attack
role.
The three initial prototypes were converted from existing Mirage
fighters and had non-retractable canards "moustaches". One of these
prototypes was nicknamed "
Asterix", after
the internationally popular French cartoon character, a tough
little Gallic warrior with a huge moustache.
A fully equipped prototype rebuilt from a
Mirage
IIIR flew in May 1970, and was powered by the uprated
SNECMA Atar 09K-50 engine, with 70.6 kN (15,900 lb
f)
afterburning thrust, following the evaluation of an earlier model
of this new series on the one-off
Mirage IIIC2.
The Milan also had updated avionics, including a laser designator
and rangefinder in the nose. A second fully equipped prototype was
produced for Swiss evaluation as the
Milan
S.
The canards did provide significant handling benefits, but they had
drawbacks. They blocked the pilot's forward view to an extent, and
set up turbulence in the engine intakes. The Milan concept was
abandoned in 1972, while work continued on achieving the same goals
with canards.
Mirage 3NG
Following the development of the Mirage 50, Dassault had
experimented with yet another derivative of the original Mirage
series, named the
Mirage 3NG (
Nouvelle
Génération, next generation). Like the Milan and Mirage 50,
the 3NG was powered by the Atar 9K-50 engine. The prototype, a
conversion of a Mirage IIIR, flew in December 1982.
The 3NG had a modified delta wing with leading-edge root
extensions, plus a pair of fixed canards fitted above and behind
the air intakes. The canards provided a degree of turbulent airflow
over the wing to make the aircraft more unstable and so more
maneuverable.
Avionics were completely modernized, leveraging off the development
effort for the next-generation
Mirage 2000 fighter. The Mirage 3NG
used a
fly-by-wire system to allow
control over the aircraft's instabilities, and featured an advanced
nav/attack system; new multimode radar; and a laser rangefinder
system. The uprated engine and aerodynamics gave the Mirage 3NG
impressive performance. The type never went into production, but to
an extent the 3NG was a demonstrator for various technologies that
could be and were featured in upgrades to existing Mirage IIIs and
Mirage Vs.
After
1989, enhancements derived from the 3NG were incorporated into
Brazilian Mirage IIIEs, as well as into four ex-Armée de l'Air
Mirage IIIEs that were transferred to Brazil
in
1988. In 1989, Dassault offered a similar upgrade refit of
ex-AdA Mirage IIIEs under the designation
Mirage
IIIEX, featuring canards, a fixed
in-flight refueling probe, a longer
nose, new avionics, and other refinements.
A total of 1,422 Mirage III/5/50 aircraft of all types were built
by Dassault. There were a few unbuilt variants:
- A Mirage IIIK that was powered by a Rolls-Royce Spey turbofan was offered to
the British Royal Air Force.
- The Mirage IIIM was a carrier-based variant,
with catapult spool and arresting
hook, for operation with the French Aéronavale.
- The Mirage IIIW was a lightweight fighter
version, proposed for a US competition, with Dassault partnered
with Boeing. The aircraft would have been
produced by Boeing, but it lost to the Northrop F-5 Freedom Fighter.
Balzac / Mirage IIIV
One of the offshoots of the Mirage III/5/50 fighter family tree was
the
Mirage IIIV vertical take-off and landing
(
VTOL) fighter. ("IIIV" is read "three-vee,"
not "three-five"). This aircraft featured eight small vertical
lift jets straddling the main engine.
The
Mirage IIIV was built in response to a mid-1960s NATO
specification for a VTOL strike fighter.
Mirage III ROSE
Project ROSE (Retrofit Of Strike Element) was an upgrade programme
launched by the
Pakistan Air
Force to upgrade old Dassault Mirage III and
Mirage 5 aircraft with modern avionics. In the
early 1990s the PAF procured 50 ex-Australian Mirage III fighters,
33 of which were selected after an inspection to undergo upgrades.
In the first phases of Project ROSE the ex-Australian Mirage III
fighters were fighters were fitted with new defensive systems and
cockpits, which included new HUDs, MFDs, RWRs, HOTAS controls,
radar altimeters and
navigation/attack
systems. They were also fitted with the FIAR Grifo M3
multi-mode radar and designated
ROSE I. Around 34
Mirage 5 attack fighters also underwent upgrades
designated
ROSE II and
ROSE III before Project
ROSE was cancelled. The Mirage III/5 ROSE fighters are expected to
remain in service with the PAF until replacement in the
mid-2010s.
Operators

French Mirage IIIR
Specifications (Mirage IIIE)
Image:mirageIIICfamily 1.jpg|Mirage III
CImage:MirageIIIEfamily.jpg|Mirage III E
Popular culture
The Mirage fighter aircraft series is featured in the popular
French
comic Tanguy et Laverdure.
The stories were made
into the 1967-1969 French TV
series Les Chevaliers du Ciel, and a French
feature film
Les Chevaliers du
ciel (international title Skyfighters) in 2005,
in which the Mirage 2000 is flown
instead.
See also
References
- Notes
- Dassault
- Bibliography
- Atlejees, Leephy. Armscor Film by Armscor, SABC and
Leephy Atlejees. Public broadcast by SABC Television, 1972,
rebroadcast: 1982, 1984.
- Baker, Nigel and Tom Cooper. "Middle East Database: Dassault Mirage III & Mirage
5/Nesher in Israeli Service".www.acig.org, Air Combat
Information Group Journal (ACIG), 26 September 2003. Retrieved: 1
March 2009.
- Breffort, Dominique and Andre Jouineau. "The Mirage III, 5, 50
and derivatives from 1955 to 2000." Planes and Pilots 6.
Paris: Histoire et Collections, 2004. ISBN 2-913903-92-4.
- "Cheetah: Fighter Technologies". Archimedes 12. June 1987.
- Cooper, Tom. "Middle East Database: War of Attrition, 1969-1970."
www.acig.org, Air Combat Information Group Journal (ACIG),
24 September 2003. Retrieved: 1 March 2009.
- "The Designer of the B-1 Bomber's Airframe". Wings
Magazine, Vol. 30/No 4, August 2000, p. 48.
- Donald, David and Jon Lake, eds. Encyclopedia of World
Military Aircraft. London: AIRtime Publishing, 2000. ISBN
1-880588-24-2.
- Green, William and Gordon Swanborough. The Complete Book of
Fighters. New York: Smithmark Books, 1994, ISBN
0-07607-0904-1.
- Jackson, Paul. "Mirage III/5/50 Variant Briefing". World
Air Power Journal 14, 15, 16.
- Lake, Jon. "Atlas Cheetah". World Air Power Journal
27: 42–53, Winter 1966.
- Pérez, San Emeterio Carlos. Mirage: Espejismo de la técnica
y de la política. Madrid: Armas 30. Editorial San Martin,
1978. ISBN 8-47140-158-4.
- Rogers, Mike. VTOL Military Research Aircraft. London:
Foulis, 1989. ISBN 0-85429-675-1.
- Schürmann, Roman. Helvetische Jäger. Dramen und
Skandale am Militärhimmel (in German). Zürich: Rotpunktverlag,
2009. ISBN 978-3-85869-406-5.
External links