Каталог - Оружие России 2000 c82-795
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608
PART 4 4
CLOSE-IN AIR DEFENSE
WEAPON SYSTEMS
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GROUP 14 GUIDED MISSILES
Class 1410 Guided Missile
Systems, Complete
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(;DB<, FF 2200
(D<F@A\, FF 153
Basic Characteristics
Sosna Sosna-A
Firing range, km 0 - 8.0 0 - 4.0
Target speed, m/s 0 - 500 0 - 300
Target altitude, m up to 3,500 up to 3,000
Armament eight Sosna-R missiles, 30mm -
twin-barreled air defense automatic gun
Gun rate of fire, rnd/min 2,400 2,400
Kill probability up to 0.95 up to 0.6
Day and night employment capability ensured
Power supply autonomous autonomous
Sosna-R air defense missile
Caliber, mm:
missile 71
booster motor 130
Maximum speed, m/s 1,200
Duration of flight to a range of 8 km, s 11.5
Missile launch weight, kg 26
Warhead weight, kg 5
Weight of missile
with transport launch canister, kg 36
Length, mm 2,200
Diameter, mm 153
- modular design which makes it possible to mount the
system on various platforms with a load-carrying
capacity of up to 3.5 t: towed trailers, armored carri-
ers, railway flat-cars, as well as stationary structures;
- versatile combat employment owing to the system’s
capability to be mounted on different platforms to
provide for protection of troops in various forms of
combat, in military railway trains, bridge and other sta-
tionary installations.
609
PART 4 4
CLOSE-IN AIR DEFENSE
WEAPON SYSTEMS
!
"!#$
% &' ()!$*
MODERNIZATION OF STRELA-10M
AIR DEFENSE MISSILE SYSTEM
Intended to provide the Strela-10M AD missile system
and its versions with day and night capability and oper-
ability in limited visibility conditions.
Main features:
1. Detection of aerial targets at night and in adverse
weather conditions. For this purpose, the system is
equipped with an IR camera.
2. Operational versatility. The system design allows for
installation of a newly introduced equipment on various
systems with minimum retrofitting operations. This
modernization makes it possible to defeat aerial targets
at night and in limited visibility conditions at ranges of
3 to 5 km.
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GROUP 14 GUIDED MISSILES
Class 1410 Guided Missile
Systems, Complete
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Basic Characteristics
Detection range, km 10
Field of view, deg:
wide 13 x 19
narrow 5.8 x 8.4
Type of monitor liquid-crystal display
Power consumption, W 150
Weight, kg not more than 50
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PART 4 4
CLOSE-IN AIR DEFENSE
WEAPON SYSTEMS
!
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MODERNIZED 9M37M MISSILE
The modernization of the 9M37M air defense
missile of the Strela-10M system is intended to
upgrade it to the level of the 9M333 missile of the
Strela-10M3 air defense system to significantly
enhance jamming immunity of the 9M37M missile
and its effectiveness in engaging modern aerial tar-
gets and to defeat small targets (cruise missiles,
remotely piloted vehicles, etc.).
In terms of interference immunity, the modernized mis-
sile is protected from:
- optical (thermal) jamming, the power of which
exceeds ten times and more that of the target IR
radiation;
- modulated jamming;
- barrage and selective IR decoys dispersed in series
or in salvo by the target, irrespective of the direction of
decoy dispersion.
Higher effectiveness in defeating modern targets is
ensured due to:
- an increase in the warhead weight from 3.5 to 5 kg
and improvement of the warhead rod section;
- use of a proximity 8-beam laser fuze with an adaptive
time delay (instead of a 4-beam pulsed fuze) that
enhances the warhead action reliability, especially
against pin-point targets.
The aforementioned characteristics are obtained by
equipping the 9M37M missile with components from
the 9M333 missile: a homing head, control compart-
ment, proximity fuze, warhead and safety-and-arming
mechanism instead of similar organic ones and mod-
ernizing the transport launch canister.
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PART 4. 4.
CLOSE-IN AIR DEFENSE
WEAPON SYSTEMS
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Systems, Complete
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MODERNIZATION OF ZSU-23-4
SHILKA SELF-PROPELLED AIR DEFENSE GUN MOUNT
Intended to develop two versions (ZSU-23-4M4 and
ZSU-23-4M5) of more improved self-propelled AD gun
mounts on the basis of up-to-date engineering and
technical solutions. The modernization involves
improvement of search capabilities, automation of bat-
tle performance, increase in accuracy of fire, particu-
larly at maneuvering targets, as well as equipping the
gun mount with advanced fire control systems,
replacement of a number of systems, units and assem-
blies with up-to-date, high-performance ones.
Improvement of search capabilities
The PPRU-M1 Sborka mobile aerial target reconnais-
sance and fire control post, comprising an up-to-date
aerial target acquisition radar and a data pickup and
transmission equipment, is introduced as the battery
command post into air defense units equipped with the
modernized ZSU-23-4M4 (ZSU-23-4M5) AD gun
mounts.
The target acquisition radar is a pulsed Doppler radar
operating on the C waveband at five fixed frequencies
with digital signal processing.
The radar is protected from passive jamming, wide-
band varying and asynchronous pulse jamming, anti-
radar missiles and can determine a jammer azimuth.
The radar is provided with a built-in system to monitor
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PART 4 4
CLOSE-IN AIR DEFENSE
WEAPON SYSTEMS
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radar serviceability
and its main para-
meters, as well as
with a simulator of
targets, jamming
sources and IFF
symbols for training
and drill of
operators.
The PPRU-M mobile
aerial target recon-
naissance and fire
control post makes
it possible, while
stationary or on the
move, to conduct
aerial target recon-
naissance (detec-
tion and identifica-
tion) and receive
aerial target data
from other reconnaissance assets.
Combat control automation
To enhance combat control effectiveness, the PPRU-M
post is modernized by replacing the data pickup and
transmission equipment with a multifunctional digital
control hardware/software complex.
The modernized PPRU-M1 post solves the following
tasks in the automatic operating mode:
- automatic pickup of coordinates of aerial targets
detected by its own target acquisition radar;
- switch-over to target tracking mode;
- automatic tracking of up to 63 targets;
- collection of data from the ZSU air defense mounts on
their location, combat readiness, ammunition status,
target tracking and engagement;
- identification of data received from its own radar and
ZSU mounts;
- delivery of target designation, responsibility sector
and fire interdiction commands to the ZSU air defense
mounts via coded telemetry channels;
- representation of data about target distribution, sec-
tors of responsibility and fire interdiction commands, as
well as information about location and status of the ZSU
mounts on the air situation displays.
The modernized PPRU-M1 post ensures, while station-
ary or on the move, reconnaissance of aerial targets
and combat control of batteries of ZSU-23-4M4 or
ZSU-23-4M5 self-propelled AD gun mounts (up to six
mounts) in the automatic operating mode.
Basic Characteristics
Target detection range, km:
at altitude of 500 m and higher up to 34
at altitude of 25 m up to 22
Clutter suppression coefficient, dB at least 30
Antenna scan rate, rpm 30
Antenna pattern width, deg:
in horizontal plane 1.6
in lower beam vertical plane 5.5
in upper beam vertical plane 30
GROUP 14 GUIDED MISSILES
Class 1410 Guided Missile
Systems, Complete
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613
PART 4. 4.
CLOSE-IN AIR DEFENSE
WEAPON SYSTEMS
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ZU-23M AIR DEFENSE GUN MOUNT
Intended to engage aerial targets at ranges of up to
2,500 m and altitudes of up to 1,500 m and defeat
lightly armored ground (waterborne) targets at ranges
of up to 2,000 m.
The modernization of the ZU-23 ensures:
- aiming automation;
- capability to engage targets flying at higher speeds;
- increase in effectiveness of fire at aerial/ground
targets;
- day and night operation capability;
- reduction of the crew by one member.
The modernization involves:
- equipping the air defense gun mount with electro-
mechanical gun-laying drives;
- replacement of the optical sight with an optronic tar-
get search and tracking system comprising a TV cam-
era, heat seeking camera, and laser rangefinder;
- introduction of a collimating sight with a built-in video
monitoring device;
- equipping the gun mount with a digital computer.
Basic Characteristics
ZU-23 ZU-23M
Guidance system manual semiautomatic +
automatic
Gun laying rate, deg/s:
traverse 30/70 90
elevation 40/70 90
Tracking accuracy, arcmin up to 30 up to 5
Aggregate accuracy of lead angle
computation and followup, arcmin up to 30 up to 3
Target speed, m/s 0 - 50 0 - 200
Kill efficiency up to 0.023 up to 0.3
Night operation not ensured ensured
GROUP 14 GUIDED MISSILES
Class 1410 Guided Missile
Systems, Complete
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614
PART 4. 4.
CLOSE-IN AIR DEFENSE
WEAPON SYSTEMS
!
"!#$
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GROUP 14 GUIDED MISSILES
Class 1410 Guided Missile
Systems, Complete
14 !
! ( !#)
:;<< 1410 =;>?@AB? C >D<ECF?<>C? <C<@?EB (>DEH:?><B)
ZU-23M1 AIR DEFENSE MISSILE-GUN MOUNT
Intended to engage aerial targets at ranges of up to
5,200 m and altitudes of up to 3,500 m by missile and
gun fire and defeat lightly armored ground (waterborne)
targets by gun fire at ranges of up to 2,000 m.
The modernization of the ZU-23 ensures:
- conversion of the air defense gun mount into the air
defense missile-gun mount;
- aiming automation;
- capability to engage targets flying at higher speeds;
- increase in effectiveness of fire at aerial and ground
targets;
- day and night operation capability;
- reduction of the crew by one member.
The modernization involves:
- installation of two launchers for firing the Igla and
Igla-1 air defense missiles;
- equipping the mount with electromechanical weapon-
laying drives;
- replacement of the optical sight with an optronic tar-
get search and tracking system comprising a TV cam-
era, heat seeking camera, and laser rangefinder;
- introduction of a collimating sight with a built-in video
monitoring device;
- equipping the mount with a digital computer.
Basic Characteristics
ZU-23 ZU-23M1
Guidance system manual semiautomatic +
automatic
Weapon laying rate, deg/s:
traverse 30/70 90
elevation 40/70 90
Tracking accuracy, arcmin up to 30 up to 5
Aggregate accuracy of lead angle
computation and followup, arcmin up to 30 up to 3
Target speed, m/s 0 - 50 0 - 360
Kill efficiency up to 0.023 up to 0.5
Night operation not ensured ensured
56 7 5-23!1
d?eA;fA;F?A; e:g hDdihB < jDfeklABEC m?:gEC A; e;:iAD-
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615
PART 4. 4.
PORTABLE AIR DEFENSE
MISSILE SYSTEMS
!
GROUP 14 GUIDED MISSILES
Class 1410 Guided Missile
Systems, Complete
14 !
! ( !#)
3455 1410 46789:7 ; 6<5=;>756;7 5;587=: (6<=@3765:)
%&'(&)* +,-,./*-0%/0.0
;@: @<B4C47=:D E737F 54=<378: , G7B8<378:, H!,
I:5<84 @<B4C47=:D E737F, = 10 - 3500
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6<B<58L @<B4C47=:D E737F 94 6NB54D, =/5:
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79;894V B46784 (9 39):
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=4554, 6R 10,6
5B7Q9VV 56<B<58L @<3784, =/5 570
8;@ R<3<G6; 54=<94G7Q79;V 87@3<G4V, 537QV[4V, @455;G94V
S<7G4V >458L <56<3<>9<-\NR4594V
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GB7=V 54=<3;6G;Q4E;; ]^, 5 14 - 17
Basic Characteristics
Targets tactical aircraft,
helicopters, RPVs and cruise missiles
Target engagement altitude, m 10 - 3,500
Target engagement range, m 500 - 5,200
Target speed, m/s:
head-on up to 360 - 400
pursuit up to 320
Weight of combat components, kg:
in combat configuration 17
in traveling configuration 18.8
Time into action, s up to 13
Reaction time, s up to 5
Operating temperature range,
0
C from -40 to +50
AD missile (9M39):
caliber, mm 72
length, mm 1,574
weight, kg 10.6
mean flight velocity, m/s 570
homing head thermal, passive
warhead HE fragmentation
fuze impact, penetration
warhead self-destruction time, s 14 - 17
; <; ;
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377 NVWG;=:7 q37=798: 6<958BN6E;; E73;.
IGLA AIR DEFENSE PORTABLE
MISSILE SYSTEM
Intended to engage low-flying targets on head-on and
pursuit courses in clutter and IR jamming environments.
The Igla system comprises a missile kept in a launch
tube with a power supply source, a launch mechanism,
training aids and maintenance facilities.
The system features automatic input of lead and ele-
vation angles, in-depth detonation of the warhead,
detonation-capable propellant in the propulsion unit
and a bias circuit in the homing head that ensures a
hit at the most vulnerable target elements.
616
PART 4. 4.
PORTABLE AIR DEFENSE
MISSILE SYSTEMS
DJIGIT SUPPORTABLE MISSILE LAUNCHER
Intended for single and salvo launch of the Igla and
Igla-1 air defense missiles.
The supportable launcher can be deployed on the
ground, in a trench, on a motor vehicle platform or
ship’s deck.
Launcher basic features
The Djigit launch complex, using the design features
of the Igla and Igla-1 air defense missiles, boasts
unique capabilities to fire two missiles in a salvo (in
addition to single missile firing) at one target that
makes it possible to increase kill probability 1.5 times
on the average.
The deployment of the launcher on a motor vehicle
increases the AD system’s mobility. The launcher
increases the number of firing channels per firer
and decreases the firer’s fatigue during combat
duty.
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GROUP 14 GUIDED MISSILES
Class 1410 Guided Missile
Systems, Complete
4),(( 14 )->*?> 3 -'@3>-3>
3>@? (-'@(B>-?)
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617
PART 4. 4.
PORTABLE AIR DEFENSE
MISSILE SYSTEMS
GROUP 14 GUIDED MISSILES
Class 1410 Guided Missile
Systems, Complete
4),(( 14 )->*?> 3 -'@3>-3>
3>@? (-'@(B>-?)
HEPP 1410 EQBRDSB K QJPXKGBPQKB PKPRBXS (QJXMHBQPS)
The launcher can be:
- disassembled into three components, carried to and
deployed at a required firing position;
- folded that significantly decreases its overall dimen-
sions and ensures concealment;
- completed with a night sight, target designator, IFF
system and other equipment.
Provision is made for training facilities and maintenance
and test equipment.
Basic Characteristics
Number of missiles:
on launcher 2
in vehicle body racks (transportable version) 6
Combat crew 1
Firing modes single or salvo firing at approaching
and receding targets
Operation mode automatic or manual
Laying angles, deg:
azimuth 360
elevation from -10 to +70
Reloading time, min 2.5 - 3
Operating temperature range, °C from -44 to +50
Weight, kg:
truck-mounted (with ammunition load
and vehicle body equipment) 320
on ground 105
Overall dimensions, mm:
on ground:
diameter across supports 2,315
height:
with canopy 1,520
in folded position (with canopy) 880
width of tipping part 1,200
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