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vakia. Other countries including Libya, Syria, Egypt, India, Cuba, Algeria, Iraq, Af-
ghanistan and North Korea have imported FLOGGERS.
The MiG-23 series served as fighter-interceptors, with a secondary capability
of ground attack. The MiG-23BN and MiG-27 were fighter-bomber variations. The
Flogger B is a standard interceptor
1
. Other versions of this aircraft are: C—two
seater; G~improved interceptor; and E—export. The MiG-23MLD FLOGGER K
version was a modification of the MiG23ML FLOGGER G and incorporated
improved avionics, armament, and aerodynamic features. The MiG-23MLD is the
most advanced version of the Flogger. It features a different identification-friend-or-
foe system, a more advanced missile capability and a distinctive notch in the leading
edge of the wing to improve flight characteristics. More than 4,000 MiG-23/27s are
estimated to have been built.
The wings are high-mounted, variable, swept-back, and tapered with blunt
2
tips. There is one turbofan engine inside the body. There are rectangular, box-like air
intakes forward of the wing roots and a single exhaust. The fuselage is long and tubu-
lar, except where intakes give a box-like appearance. It has a long, pointed nose and a
stepped canopy. There is a large, swept-back, and tapered belly fin under the rear sec-
tion. The tail is swept-back, has a tapered tail fin, has a curved dorsal
3
in the leading
edge and an angular tip. Swept-back, tapered flats have angular tips and are high-
mounted on the fuselage. The MiG-23UB is a two-seat combat trainer version of the
MiG-23 third generation interceptor-fighter. It was fitted with a variable sweep wing
and this feature helped solve the problems of the multi-role combat aircraft capable
of performing front-line fighter, interceptor-fighter
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and low altitude fighter-bomber
missions. The decision on the development of the combat trainer was taken two years
after the first MiG-23 prototype was manufactured at the end of 1967. The MiG-
27UB is a day and night all-weather combat trainer that can carry various armaments,
including the GSh-23L gun, rockets, bombs, the R-3S air-to-air and Kh-23 air-to-
surface missiles.
The development of the two-seater, dubbed "23-51", was made in March 1969,
and in May, it made the first flight (Design Bureau's test pilot M.M. Komarov). The
MiG-23UB state tests were completed in 1970 and the aircraft entered the service, so
the IAIA launched the production run.
The first MiG-23UB was produced on the basis of the MiG-23C one-seater.
The changes were made in the nose fuselage up to frame No. 18. The fuel tank No.l
was decreased to place co-pilot seat and the 470- litre fuel tank was located in the tail
fuselage.
The first production aircraft was tested by Moscow test pilot A.V. Fedotov to-
gether with the factory test pilot E.N. Tcheltsov. Later on, the aircraft were tested by
V.S. Prantskyavitchus, N.N. Ivanov, G.E. Bulanov, G.M. Kurkai, E.M.
1
interceptor - интерцептор
2
blunt - тупой
3
dorsal - задний
4
interceptor-fighter – истребитель-перехватчик
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