Tu-22M
Backfire
PHOTO
GALLERY
NATO
reporting name: 'Backfire'
TYPE:
Twin-engined variable geometry
medium bomber and maritime reconnaissance/attack aircraft.
PROGRAMME:
"NATO revealed the existence
of a Soviet variable geometry bomber programme autumn 1969; prototype observed
July 1970 on the ground near Kazan manufacturing plant, western Russia;
confirmed subsequently as twin-engined design by Tupolev OKB; at least two
prototypes built, with first flight estimated 1969, up to 12 pre-production
models by early 1973, for development testing, weapons trials and evaluation;
production has been 30 a year.
DESIGN FEATURES:
Capable of performing nuclear
strike, conventional attack and anti-ship missions; low-level penetration
features ensure better survivability than for earlier Tupolev bombers; not
expected to become ALCM carriers, although used for development launches,
deployment of RKV-500B (AS-16 'Kickback') short-range attack missiles in Tu-22Ms
has increased significantly their weapon carrying capability. Low/mid-wing
configuration; large-span fixed center-section and two outer steering sleeves
variable from 20 degrees to 65 degrees sweepback; no anhedral or dihedral, but
wing section so thin that outer panels flex considerably in flight; leading-edge
fence towards tip of section-section each side; basically circular fuselage
forward of wings, with ogival dielectric nosecone; fuselage-fuselage faired into
rectangular section air intake trunks, each with large splitter plate and
assumed to embody complex variable geometry ramps; no external area ruling of
trunks; all-swept tail surfaces, with large dorsal fin.
LANDING GEAR:
Retractable tricycle type; each
mainwheel bogie comprises three pairs of wheels in tandem, with two forward
pairs farther apart than rear pairs; bogies pivot inwards from vestigial fairing
under section-section on each side into bottom of fuselage.
POWER PLANT:
Two unidentified turbofans, side
by side in rear fuselage, each more than 2500 kg with afterburning. Fuel is in
integral tanks in wing central section and steering sleeves and in fuselage
tanks.
ACCOMMODATION:
Pilot and co-pilot side by side,
under upward opening gull-wing doors hinged on centreline; two crew members
further aft, as indicated by position of windows between flight deck and air
intakes.
AVIONICS:
Large missile targeting and
navigation radar (NATO 'Down Beat') inside dielectric nosecone; radar ('Box
Tail') for tail turret, above guns. Fairing with flat glazed front panel under
front fuselage, for video camera to provide visual assistance for weapon aiming
from high altitude. Very advanced ECM and ECCM; infrared missile approach
warning sensor above fuselage aft of cockpit; eight chaff/flare multiple
dispensers in bottom of each engine duct between wingroot and tailplane, another
in each tailplane root fairing.
ARMAMENT:
Max offensive weapon load three
Kh-22 (NATO AS-4 'Kitchen') air-to-surface missiles, one semi-recessed under
fuselage-fuselage, one under fixed section-section panel of each wing; or 24,000
kg (52,910 lb) of conventional bombs or mines, half carried internally and half
on racks under wings and engine air intake trunks. Internal bombs can be
replaced by rotary launcher for six Kh-15P (AS-16 'Kickback') short-range attack
missiles, with four more underwing as alternative to Kh-22s. Normal weapon load
is single Kh-22 or 12,000 kg (26,455 lb) of bombs. Typical loads two FAB-3000,
eight FAB-1500, 42 FAB-500 or 69 FAB-250 or -100 bombs (figures indicated weight
in kg), or eight 1500 kg or 18 500 kg mines. One GSh-23 twin-barrel 23 mm gun,
with barrels superimposed, in radar directed tail mounting."
DIMENSIONS
EXTERNAL (Tu-22M-3)
|
Wingspan
|
fully
spread: 34.28 m (112 ft 5 3/4 in)
|
fully
swept
|
23.30
m (76 ft 5 1/2 in)
|
Wing
aspect ratio
|
fully
spread: 6.40
|
fully
swept
|
3.09
|
Length
overall
|
42.46
m (139 ft 3 3/4 in)
|
Height
overall
|
11.05
m (36 ft 3 in)
|
Weapons
bay
|
Length
approx 7.00 m (22 ft 11 1/2 in)
|
Width
|
approx
1.80 m (5 ft 10 3/4 in)
|
WEIGHTS
AND LOADINGS (Tu-22M-3)
|
Max
weapon load
|
24,000
kg (52,910 lb)
|
Fuel
load
|
approx
50,000 kg (110,230 lb)
|
Max
wing loading (without JATO)
|
20
degrees sweep
|
675.45
kg/m/2 (138.34 lb/sq ft)
|
65
degrees sweep
|
705.35
kg/m/2 (144.45 lb/sq ft)
|
Max
power loading (without JATO)
|
253
kg/kN (2.48 lb/lb st)
|
PERFORMANCE
(Tu-22M-3)
|
Max
level speed
|
at
high altitude
|
Mach
1.88 (1080 knots; 2000 km/h; 1242 mph)
|
at
low altitude
|
Mach
0.86 (567 knots; 1050 km/h; 652 mph)
|
Nominal
cruising speed at height
|
485
knots (900 km/h; 560 mph)
|
T-O
speed
|
200
knots (370 km/h; 230 mph)
|
Normal
landing speed
|
154
knots (285 km/h; 177 mph)
|
Service
ceiling
|
133,00
m (43,635 ft)
|
g
limit
|
+2.5
|
LENGTH
(m)
|
42.46
|
HEIGHT
(m)
|
11.05
|
WINGSPAN
(m)
|
34.28
|
MAX
T-O WEIGHT (kg)
|
124,000
|
MAX
WING LOAD (kg/m/2)
|
705.35
|
MAX
LEVEL SPEED (knots)
|
1080
|
SERVICE
CEILING (m)
|
13,300
|
T-O
RUN (m)
|
2100
|
LANDING
RUN (m)
|
1300
|
(source: Jane's)
Tupolev Tu-22M
Country of origin. Russia
Type. Strategic and maritime
strike/reconnaissance bomber
Powerplants. Tu-22M-3 - Two 245.2kN (55,115lb) with afterburning Kuznetsov/KKBM
NK-25 turbofans.
Performance.- Tu-22M-3 - Max speed at high altitude Mach 1.88 or 2000km/h
(1080kt), max speed at low level Mach 0.86 or 1050km/h (567kt), normal cruising
speed at altitude 900km/h (485kt). Service ceiling 43,635ft. Supersonic combat
radius with a 12,000kg (26,455lb) weapons load 1500 to 1850km (810 to 1000nm).
Subsonic combat radius with max weapons load hi-hi-hi 2200km (1190nm). Subsonic
combat radius with 12,000kg (26,455lb) bomb load lo-lo-lo 1500 to 1665km (810 to
900nm), or hi-lo-hi 2410km (1300nm).
Weights: Tu-22M-3 - Empty 54,000kg (119,050[b), max takeoff 124,000kg
(273,370lb), rocket assisted takeoff 126,400kg (278,660lb).
Dimensions. Tu-22M-3 - Wing span wings extended 34.28m (112ft 6in), span wings
swept 23.30m (76ft 6in), length overall 42.46m (139ft 4in), height 11.05m (36ft
3in). Wing area wings extended 183.6ml (1976.1 sq ft), wing area wings swept
175.8M2 (1 892.4sq ft). Accommodation. Crew of four with pilot and copilot side
by side, with navigator and weapons systems operator behind them.
Armament: One GS11-23 twin barrel 23mm cannon in the tail. Can carry 24,000kg
(52,910lb) of conventional bombs or mines in bomb bay, or six Kh-15P (AS-16
'Kickback') ASMs on a rotary launcher in bomb bay and four underwing, or three
Kh-22 (AS-4 'Kitchen') ASMs, one semi recessed under fuselage and one on each
underwing hardpoint.
Operators. Russia, Ukraine.
History. The Tu-22M was conceived as a swing wing conversion of the Tu-22 but
evolved into essentially an all new aircraft.
Tupolev first looked at fitting the Tu-22 with swing wings in 1961. Wind tunnel
tests revealed that fitting the Tu-22 with swing wings and a minimum of other
changes would almost double combat radius while halving field length. Design
work on this aircraft, designated Tu-22M, began in 1962, however Tupolev took
the opportunity to substantially redesign the basic Tu-22 to even further
improve performance. Apart from the swing wings the other key change was the
powerplants, two Kuznetsov NK-20 afterburning turbofans mounted in the rear of
the fuselage. The engines were fed by two F-4 style intakes with variable
splitter plates. The nose was redesigned, while new six wheel main undercarriage
units retracted into the fuselage.
The first Tu-22M-O prototype, a much converted Tu-22, first flew on August 30
1964, although the west did not identify the new bomber until September 1969.
The NATO reporting name 'Backfire-A' was subsequently adopted. Production was of
the further redesigned Tu-22M-2 (with a new nav/attack radar) and did not begin
until 1972.
About 200 Tu-22M-2 'Backfire-Bs' were built before production switched to the
Tu-22M-3, which first flew in 1980. The Tu-22M-3 is powered by two increased
thrust NK-25 turbofans fed by new wedge shaped air inlets, and introduced a new
multimode radar in a reprofiled nose and has an increased max takeoff weight.
The Tu-22MR is an ECM or EW aircraft, with about 10 in service.
Almost 500 Tu-22Ms of all models have been built."
(source: International
Directory of Military Aircraft 1998-1999)
Secondary Source: venik.way.to