Каталог - Оружие России 2000 c82-795
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PART 1 1
287
TECHNICAL SUPPORT
AND RECOVERY VEHICLES
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MTP-A2.1 TECHNICAL SUPPORT VEHICLE
The vehicle is intended to provide technical assistance
to drivers (crews) in eliminating the troubles (damages)
of the UralAZ, KamAZ, ZIL, GAZ, UAZ family trucks,
weapons and military equipment mounted on their
chassis, fill them with fuel, oil and special liquids, pull
out lightly bogged down vehicles and transport faulty
(damaged) vehicles in the half-loaded position with
damaged running and steering gears and also tow a
vehicle with no driver in its cab by using two rigid tow-
ing bars.
The vehicle’s main equipment comprises a standard
winch, hoisting gear, half-loaded vehicle transporting
facility, towing gears, anchoring spade to ensure the
maximum pull-out effort, rigging gear to pull out bogged
down vehicles, set of appliances, tools, spare parts and
materials required to make faulty (damaged) vehicles ser-
viceable or ready
for transportation,
as well as a radio
station.
The MTP-A2.1
technical support
vehicle equipment
is arranged on a
specially provided
platform frame, as
well as in recesses
and cases of racks
and a bench.
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Basic characteristics
Basic chassis URAL-4320-31
Maximum weight of cargo carried
on platform, kg 4,705
Maximum load on transport facility, kg 3,500
Maximum towed vehicle weight, kg:
half-loaded, on all roads and terrain 12,000
by towing:
on terrain 9,000
on paved roads 15,500
Gross weight with cargo on platform, kg 17,600
Maximum recovery effort, kN (tf) 137 (14)
Cargo-lifting capacity with a jib boom of, kgf:
5.4 m 1,650
3.8 m 2,300
2.1 m 4,000
Maximum crane hook height, m 8.2
Overall dimensions, mm:
length 8,510
width 2,500
height 3,300
Maximum winch tractive force used for recovery of trucks, t:
w/o winch pulley 10 - 11
with winch pulley 20
Maximum fording depth, m 1.7
GROUP 49 MAINTANANCE AND REPAIR SHOP EQUIPMENT
Class 4910 Motor Vehicle Maintenance
and Repair Shop Specialized Equipment
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PART 1 1
GROUP 49 MAINTANANCE AND REPAIR SHOP EQUIPMENT
Class 4910 Motor Vehicle Maintenance
and Repair Shop Specialized Equipment
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MOBILE MAINTENANCE AND REPAIR WORKSHOPS
(MTO-V, MTO-80, MTO-M, MTO-BT, MTO-AM, MRS-AR,
MRS-BT, MRIV AND MRM)
Intended for maintenance and running repair of arma-
ment and combat equipment.
The workshops can be operated at ambient air tem-
peratures ranging from -45 to +50 °C, relative humidi-
ty of up to 98 percent at a temperature of +25 °C, dust
content of up to 1.5 g/m
3
, wind velocity of up to
20 m/s, altitude of up to 4,000 m above sea level.
The workshop equipment enables the crew to carry out
the following operations: hoisting-and-transporting,
repair-and-bench, electric welding, electric wiring and
installation, copper-and-tin smith, joinery, painting, and
repair of electrical equipment.
The mobile workshop main equipment comprises: a
three-phase 400 V 50 Hz AC generator rated at 12 to
16 kW, storage battery charging equipment, jib crane
with a load-lifting capacity of 1.5 to 2 tf, set of equip-
ment for maintenance and repair of armament and
combat equipment, electric hand-held tools.
Auxiliary equipment: hydraulic jack; screw-cutting
machine; welding generator; equipment, tools and
devices for manual electric-arc and argon-arc welding;
fitting/mechanical tool kit; electrician’s instruments and
tool kit; small-size filling unit; filling tool kit; set of wash-
ing baths; copper/tin smith’s tool kit; tent.
Depending on their purpose, the workshops can be
equipped with special tools and appliances.
The workshops are mounted on the ZIL, KamAZ, GAZ
and Ural chassis equipped with a winch and a power
takeoff box.
The van body is intended to house the workshop equip-
ment, implements, tools and appliances, carry out
repair and accommodate the crew at work and rest. It
is made of metal framework and equipped with the
OV65 heater and FVUA-100N-24 filter-ventilation unit to
provide normal conditions for work and rest.
During organizational repair, the workshops can be
used independently or in conjunction with other main-
tenance and repair facilities, such as checkout and test
vehicles, repair stations, etc.
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288
TECHNICAL SUPPORT
AND RECOVERY VEHICLES
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PART 1 1
289
TECHNICAL SUPPORT
AND RECOVERY VEHICLES
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Basic characteristics
Chassis ZIL-131 KamAZ-43101
Van body KM-131 KM-4310
Total weight, t about 10 about 13
Number of workstations:
in van body 3 - 5
out of van body 6 - 9
Overall dimensions, mm:
length 7,470 8,270
width 2,570 2,550
height (in travelling position) 3,255 3,378
Time required to set up (close down)
the maintenance truck, min 25/30
Power supply from own generator, mobile electric
power stations, industrial power supply
mains of 400 V (380 V) 50 Hz three-phase AC
GROUP 49 MAINTANANCE AND REPAIR SHOP EQUIPMENT
Class 4910 Motor Vehicle Maintenance
and Repair Shop Specialized Equipment
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PART 1 1
290
DIESEL ENGINES
GROUP 23 GROUND EFFECT VEHICLES, MOTOR VEHICLES, TRAILERS AND CYCLES
Class 2320 Tracks
and Truck Tractors, Wheeled
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(V-8) 61L<1-5>M 180-330 +.-. 2 60-80-4 ?1:3 /-5,<,2-
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45-Q 2 6<1?1519+82<16 8-91+<4<88. 1234 X1.-8.1-
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DG-8471.10
YaMZ-8471.10
DG-7511.10
YaMZ-7511.10
DG-460
YaMZ-460
DG-7601.10
YaMZ-7601.10
YaMZ DIESEL ENGINES
FOR MILITARY EQUIPMENT
Between 1960s and 1980s, YaMZ-236 (V-6) and
YaMZ-238 (V-8) diesel engines rated at 180 - 330 hp,
produced by Avtodizel JSC (Yaroslavsky Motor Plant,
Russian acronym - YaMZ), were installed on trucks and
tracked armored vehicles (artillery towing vehicles,
armored personnel carriers, self-propelled howitzers,
air defense missiles complexes, engineer equipment).
Since 1990s, Ural trucks, BTR-80 armored personnel
carriers, and GT-TM tracked tractors have been
equipped with YaMZ engines and powerplants with
improved technical characteristics. A number of their
modifications are manufactured in a multifuel version.
New uprated modifications of the YaMZ family engines
are: YaMZ-7601 (V-6) rated at 230 - 300 hp and
YaMZ-7511 (V-8) rated at 300 - 420 hp meet the
requirements of the Euro-1 and Euro-2 international
ecological standards.
Military derivative engines YaMZ-847 (V-12) rated at up
to 800 hp, YaMZ-846 and YaMZ-849 (V-8) rated at up
to 500 hp have been developed from the 840-family
YaMZ engines to equip MZKT (Minsk), KZKT (Kurgan)
and BAZ (Bryansk) multiaxle prime movers and special-
purpose chassis, as well as IZTM (Ishimbai) tracked
vehicles. The design of these engines features a high
uprating, leakproofness of accessories, multifuel opera-
tion, ability to run at an altitude of 4,500 m and an elec-
tronic system to monitor engine operation and protect it
in emergency. All versions of the 840-family engines are
provided with gas turbine supercharging and water-to-
air intermediate cooling of supercharged air.
DG-238G2-6
YaMZ-238G2-6
PART 1 1
291
DIESEL ENGINES
GROUP 23 GROUND EFFECT VEHICLES, MOTOR VEHICLES, TRAILERS AND CYCLES
Class 2320 Tracks
and Truck Tractors, Wheeled
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DG-236G2-4 V-6 130 R 140 132 (180) 2100 667 (68) 1250-1450 214 (157) 1185 «U.,+-43206»
DG-238G2-6 V-8 130 R 140 176 (240) 2100 883 (90) 1250-1450 214 (157) 1390 «U.,+-4320-30(31)»
DG-238G2-7 V-8 130 R 140 176 (240) 2100 883 (90) 1250-1450 214 (157) 1390 -5926 (VW-80)
DG-238-1 V-8 130 R 140 220 (300) 2100 1079 (110) 1450-1600 - 1210 G-V/, 2v1
DG-238V V-8 130 R 140 228 (310) 2000 1207 (123) 1200-1400 208 (153) 1580 *.-6322
DG-238V-8 V-8 130 R 140 220 (300) 2000 1180 (120) 1200-1400 204 (150) 1530 «U.,+-5323»
DG-238V-15 V-8 130 R 140 220 (300) 2000 1180 (120) 1200-1400 204 (150) 1565 V-69506
(507, 508), 69531
DG-8401.10-14 V-12@ 140 R 140 478 (650) 2100 2450 (250) 1300-1500 204 (150) 1840 **-74281,
G*-74131
DG-8401.10-24 V-12@ 140 R 140 478 (650) 2100 2450 (250) 1400-1600 208 (153) 1840 G*-7413
DG-846 V-8@ 140 R 140 367 (500) 2100 1960 (200) 1200-1400 203 (149) 1450 G*
DG-849 V-8@ 140 R 140 367 (500) 2100 1960 (200) 1200-1400 203 (149) 1450 V
wWvw* DG
DG-7511.10 V-8 130 R 140 294 (400) 1900 1715 (175) 1100-1300 194 (143) 1685 G, *., «U.,+»
DG-7601.10 V-6 130 R 140 220 (300) 1900 1330 (130) 1100-1300 194 (143) 1350 G, *., «U.,+»
DG-847.10 V-12@ 140 R 140 588 (800) 2100 3087 (315) 1400-1500 203 (149) 1950 G*-79221,
**-74281
DG-8471.10 V-12@ 140 R 140 588 (800) 2100 3087 (315) 1400-1500 203 (149) 1950 G -30wG
DG-460 W-4@ 102 R 122 125 (170) 2400 634 (62) 1300-1500 206 (152) 400 -3308,
-39371
(«1:<8;») 8 :..
- 5/.71<,::/2
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Basic Characteristics
Model, Type Piston Power, Speed, Maximum Engine speed Minimum Weight, Installed
build-up diameter kW (hp) rpm torque, at maximum specific fuel kg on motor
and stroke, N
.
m (kgf
.
m) torque, rpm consumption vehicles
mm rate, g/kW
.
h
(g/hp
.
h)
YaMZ-236G2-4 V-6 130 R 140 132 (180) 2,100 667 (68) 1,250-1,450 214 (157) 1,185 Ural-43206
YaMZ-238G2-6 V-8 130 R 140 176 (240) 2,100 883 (90) 1,250-1,450 214 (157) 1,390 Ural-4320-30(31)
YaMZ-238G2-7 V-8 130 R 140 176 (240) 2,100 883 (90) 1,250-1,450 214 (157) 1,390 GAZ-5926 (BTR-80)
YaMZ-238N-1 V-8 130 R 140 220 (300) 2,100 1,079 (110) 1,450-1,600 - 1,210 G-LBu, 2S1
YaMZ-238BL V-8 130 R 140 228 (310) 2,000 1,207 (123) 1,200-1,400 208 (153) 1,580 KrAZ-6322
YaMZ-238B-8 V-8 130 R 140 220 (300) 2,000 1,180 (120) 1,200-1,400 204 (150) 1,530 Ural-5323
YaMZ-238B-15 V-8 130 R 140 220 (300) 2,000 1,180 (120) 1,200-1,400 204 (150) 1,565 BAZ-69506
(507, 508), 69531
YaMZ-8401.10-14 V-12C 140 R 140 478 (650) 2,100 2,450 (250) 1,300-1,500 204 (150) 1,840 KZKT-74281,
MZKT-74131
YaMZ-8401.10-24 V-12C 140 R 140 478 (650) 2,100 2,450 (250) 1,400-1,600 208 (153) 1,840 MZKT-7413
YaMZ-846 V-8C 140 R 140 367 (500) 2,100 1,960 (200) 1,200-1,400 203 (149) 1,450 GZ*
YaMZ-849 V-8C 140 R 140 367 (500) 2,100 1,960 (200) 1,200-1,400 203 (149) 1,450 BAZ
ADVANCED YaMZ ENGINES
YaMZ-7511.10 V-8 130 R 140 294 (400) 1,900 1,715 (175) 1,100-1,300 194 (143) 1,685 MAZ, KrAZ, Ural
YaMZ-7601.10 V-6 130 R 140 220 (300) 1,900 1,330 (130) 1,100-1,300 194 (143) 1,350 MAZ, KrAZ, Ural
YaMZ-847.10 V-12C 140 R 140 588 (800) 2,100 3,087 (315) 1,400-1,500 203 (149) 1,950 GZ*-79221,
*Z*-74281
YaMZ-8471.10 V-12C 140 R 140 588 (800) 2,100 3,087 (315) 1,400-1,500 203 (149) 1,950 IZTM D-30PM
YaMZ-460 R-4C 102 R 122 125 (170) 2,400 634 (62) 1,300-1,500 206 (152) 400 GAZ-3308,
GAZ-39371 (Vodnik)
and others
- turbocharged
C - turbocharged, with cooling of supercharged air
294
PART 2 2
BOMBER AIRCRAFT
GROUP 15 AIRCRAFT AND AIRFRAME
STRUCTURAL COMPONENTS
Class 1510 Aircraft, Fixed Wing
15 ! !
" #$ ! " %##$
+,-- 1510 .,/0+123
Tu-160 SUPERSONIC STRATEGIC
MISSILE-CARRYING BOMBER
The Tu-160 bomber is intended to defeat the most
important targets in far-off military-geographic
areas and in the deep rear of continental theaters of
operations by using nuclear and conventional
weapons.
The bomber’s airframe is of an integrated configu-
ration featuring a blended wing-body layout. The
peculiarity of the airframe structure resides in a tita-
nium beam which is an all-welded torsion box pro-
vided with outer wing panel tilting assemblies. All
the main airframe members are secured on this lon-
gitudinal beam running through the entire airframe.
The variable-geometry (from 20° to 65°) wing
assures high aerodynamic characteristics at both
supersonic and subsonic speeds alike.
The aircraft is equipped with all-moving vertical and
horizontal tail surfaces. It features a fly-by-wire con-
trol system.
The Tu-160 bomber is powered by four augmented tur-
bofan engines arranged in two engine nacelles and
provided with variable vertical wedge air intakes.
The bomber is equipped with an in-flight refueling sys-
tem provided with an extendible refueling probe
arranged in the nose fuselage in front of the pilots’
cockpit.
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1#!
AIRCRAFT
295
PART 2 2
BOMBER AIRCRAFT
GROUP 15 AIRCRAFT AND AIRFRAME
STRUCTURAL COMPONENTS
Class 1510 Aircraft, Fixed Wing
15 ! !
" #$ ! " %##$
+,-- 1510 .,/0+123
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The crew occupies K-36LM ejection seats enabling
the crewmembers to escape from the aircraft in an
emergency at all altitudes and airspeeds, including
zero values.
The Tu-160’s avionics comprises an integrated aim-
ing, navigation and flight control system; airborne
radar; ECM equipment; automatic control system;
and other equipment. It ensures the execution of
flight missions at any time of the day, in all weather
conditions and throughout the entire range of geo-
graphic latitudes.
The aircraft features a highly computerized airborne
equipment.
The cockpit data display system is represented by
electromechanical dispalys and monitors. The con-
trol columns, which are traditional for large aircraft,
are replaced here by the fighter type control sticks.
The Tu-160 bomber’s armament comprises subson-
ic nuclear-tipped long-range cruise missiles. The
missiles are arranged on multistation launchers, six
missiles in each of the two weapon bays. Provision
is also made for aerial bombs of various purpose
and types with a total weight of up to 40 t.
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m,Q,HP2J31 H,K/1H3
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,HY, ISPW,21+M, Y0+-S0 T 2MW,, YW- n-32, 4 T 25000
Basic Characteristics
Crew 4
Maximum takeoff weight, t 275
Normal/maximum combat load, t 9/40
Fuel weight, t 148
Operational flight range
with normal/maximum combat load, km over 12,500/10,500
Maximum flight speed, km/h:
at altitude 2,200
near ground 1,030
Service ceiling, m 15,000
Required concrete runway length, m 3,050
Overall dimensions
(length x height x wing span), m 54.1 x 13.1 x 55.7/35.6
Engine type, number x thrust, kgf NK-32, 4 x 25,000
296
PART 2 2
BOMBER AIRCRAFT
GROUP 15 AIRCRAFT AND AIRFRAME
STRUCTURAL COMPONENTS
Class 1510 Aircraft, Fixed Wing
15 ! !
" #$ ! " %##$
+,-- 1510 .,/0+123
Tu-22M3 LONG-RANGE
MISSILE-CARRYING BOMBER
The Tu-22M3 long-range missile-carrying bomber is
designed to defeat optically visible and radar contrast,
single and area, ground and sea, mobile and stationary
targets with supersonic air-to-ground missiles and aer-
ial bombs in the operational and strategic depth of
enemy defenses by day and night, in any season, in
VFR and IFR weather conditions.
The Tu-22M3 retained the variable-sweep wing of its
precursor (Tu-22M2). Its flight performance upgrading
has been achieved owing to the weight-saving struc-
ture design, advanced aerodynamic configuration, as
well as new, more fuel-efficient and powerful engines.
The new powerplant is able to ensure single-engine
level flight and landing. On the ground the engines can
be started autonomously from an auxiliary power unit.
Its onboard equipment, incorporating an integrated
flight control and navigation system, a radar, an opti-
cal/TV automatic bomb sight, an automatic flight con-
trol system, and a missile weaponry control system,
ensures an automated execution of navigational, aiming
and piloting tasks during preset or expeditiously intro-
duced program-assisted flight, as well as bombing and
missile launching problems.
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297
PART 2 2
BOMBER AIRCRAFT
GROUP 15 AIRCRAFT AND AIRFRAME
STRUCTURAL COMPONENTS
Class 1510 Aircraft, Fixed Wing
15 ! !
" #$ ! " %##$
+,-- 1510 .,/0+123
The Tu-22M3 air-
craft armament is
arranged inside the
fuselage and on four
external-store hard-
points. It comprises:
- one to ten air-to-
surface, air-to-ship
and air-to-radar
cruise missiles;
- up to 24 tons of
aerial bombs and
mines.
To protect the
bomber’s aft hemi-
sphere against
enemy fighters’
attacks, the aircraft
is provided with one
23mm gun mount
installed in the aft
fuselage.
To enhance combat
survivability and
flight safety, the
bomber is equipped
with the following
systems:
- fuel tank inert gas
system;
- firefighting system
to protect engine
compartments, aux-
iliary power unit, ser-
vice compartments,
as well as fuselage
and wing fuel tanks;
- KT-1 ejection seats enabling the crew to abandon the
aircraft in emergency from zero altitude to the service
ceiling.
The hydraulic equipment is built around three indepen-
dent systems.
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,GP, HQOZ,21+L, P0+-Q0 R 2LZ,, PZ- a-25, 2 R 25000
Basic Characteristics
Crew 4
Weight, t:
aircraft:
maximum takeoff 124
normal landing 78
combat load:
normal 6
maximum 24
fuel 53
Combat radius, km 2,200
Maximum flight speed, km/h 2,000
Takeoff run, m 2,000 - 2,100
Aircraft overall dimensions
(length x height x wing span), m 42.5 x 11.1 x 23.3/34.28
Engine type, number x thrust, kgf NK-25, 2 x 25,000
300
PART 2 2
FIGHTER-BOMBERS -
GROUP 15 AIRCRAFT AND AIRFRAME
STRUCTURAL COMPONENTS
Class 1510 Aircraft, Fixed Wing
15 ! !
" #$ ! " %##$
1233 1510 2451678
Su-17M4 (Su-22M4) FIGHTER-BOMBER
The Su-17M4 variable-geometry-wing fighter-bomber
is designed to penetrate enemy air defenses at low
altitudes, destroy stationary and moving ground tar-
gets (including pinpoint and high-strength ones) by
missiles, unguided aerial bombs, rocket projectiles and
gun armament from extreme low, low and medium alti-
tudes in visual flight conditions; defeat operating
ground radars by missiles; and engage aerial targets in
visual flight conditions (a subsidiary mission).
The Su-17M4 is developed from the serially-produced
Su-17M3 fighter-bomber with due account for the
combat use and operation of the Su-20 and Su-22 air-
craft (export versions of the Su-17). The Su-17M4 fea-
tures an extended armament complement and a mod-
ernized PrNK-54 aiming and navigation digital complex
comprising a weapon control system, a target illumi-
nating and ranging station, a short-range radio naviga-
tion system, a digital computer, a Doppler velocity and
drift meter and an inertial heading and attitude refer-
ence system.
In addition, the Su-17M4 is provided with an upgraded
automatic flight control system and an improved radio
set. The aircraft features enhanced survivability due to
modernized ECM equipment and radar illumination
warning station.
The Su-17M4 fighter-bomber armament system com-
prises the following weapons:
- Kh-25ML, Kh-29L, Kh-29T and S-25L air-to-surface
missiles;
- Kh-58U, Kh-27PS and Kh-25MP air-to-radar missiles;
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