|
Entered service |
1973 |
|
Crew |
2 men |
|
Dimensions and weight |
|
Length |
22.59 m |
|
Wing span |
17.64
m spread, 10.37 m swept |
|
Height |
6.19
m |
|
Weight (empty) |
22.3 t |
|
Weight (maximum take off) |
36 t |
|
Engines and performance |
|
Engines |
2 x Perm / Sploviev AL-21F-3A turbojets |
|
Traction (with afterburning) |
2 x 109.83 kN |
|
Maximum speed |
1 320 km/h |
|
Service ceiling |
17 km |
|
Combat radius |
560 - 1 250 km |
|
Armament |
|
Cannon |
1 x 23-mm cannon |
|
Missiles |
Kh-23, Kh-25ML, Kh-29L/T, Kh-59 Ovod
air-to-surface missiles; Kh-25MP, Kh-31P, Kh-29MP and Kh-58 anti-radar
missiles; Kh-31A, Kh-35 anti-ship missiles, R-60 air-to-air missiles |
|
Bombs |
TN-1000 and TN-1200 free-fall nuclear weapons,
KAB-500Kr laser guided bombs |
|
The Su-24
remains a powerful long-range, low-level strike attack aircraft with
real all-weather precision attack capability. With its variable
geometry swing wing and side-by-side cockpit, the Su-24 is
inevitably compared with the US General Dynamics
F-111. The aircraft
was never intended or used as a strategic bomber, however, a fact
obscured by such comparisons. The Su-24 is more broadly equivalent
to the Anglo-German-Italian Tornado.
The Fencer
was designed to replace the Yak-28 in the all-weather low-lever
tactical strike and attack roles. It was intended to carry free-fall
TN-1000 and TN-1200 nuclear bombs, and a variety of conventional
free-fall bombs, rockets and guided air-to-surface missiles to attack fixed and mobile
targets with pinpoint accuracy. While optimized as a supersonic
bomber the aircraft was also intended to have a secondary
photographic reconnaissance role, and to replace the Brewer in the
electronic warfare role.
The design
of what became the Sukhoi Su-24 began in the early 1960s. Sukhoi,
however, abandoned its initial design (an enlarged, twin-engined
aircraft based loosely on the Su-7 configuration, but with a tandem
cockpit) in favour of the compound Delta T6. This featured
fuselage-mounted lift jets for enhanced STOL performance. The lift
jets were heavy and bulky, however, and the T6 was redesigned six
months later.
The
resulting T-6-21G prototype had no lift jets (leaving increased
space for fuel and weapons) but did feature a VG swing wing. This
was added to improve take-off and landing performance. The aircraft
made its maiden flight during May 1970 and was ordered into
production as the Su-24 in late 1970.
The
production Su-24 entered frontline service in 1973. The Su-24 was
deployed with the Group of Soviet Forces in Germany in 1979, and in
Poland. From 1984 the Su-24 saw active service in Afghanistan.
The original
Su-24 underwent slight changes in configuration during production,
and this led NATO's ASCC to assign three reporting names (Fencer-A
through to -C). The aircraft was fast and stable at low level, and
could carry an impressive warload (though only at the expense of
range) but its avionics were backward and unreliable. The aircraft
was thus never as capable as Western attack aircraft.
The improved
Su-24M Fencer-D was a much better aircraft, and entered service in
1986. The Su-24M introduced upgraded avionics, with separate Orion-A
forward-looking attack and Relief Terrain Following Radars. It also
had a Kaira 24 laser and TV sighting system which gave PGM
compatibility. The Fencer-D had a retractable refuelling probe above
the nose, and could carry a buddy refuelling store on the
center-line. At least 670 Su-24s have definitely been built. The
overall total is probably between 900 - 1 200. Fencer-Bs, -Cs, -Ds
and -Es remain in wide-spread front line use in Russia, and various
former Soviet states. Downgraded, non-nuclear capable export
Su-24MKs have been delivered to Algeria, Iran, Iraq, Libya and
Syria.
A proposed
replacement for the ageing Su-24s is a new
Su-34 long-range interdictor, which is a derivative of the
Su-27 air superiority fighter. It has been accepted to service
with the Russian air force, however due to funding restrictions only
few of these new aircraft are operational.
|