Каталог - Оружие России 2000 c82-795
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flight; in the cruise mode, lasting up to 12 s, the
motor maintains this speed. Such a flight speed
envelope ensures the required power-to-weight
ratio, which enables the missile to cover a zone of
up to 12 km in range and defeat targets flying at a
speed of up to 700 m/s and g-loads of up to 10 g.
The missile is maintenance-free and accommodated
in a four-compartment transport launch canister.
Command/control assets
Organizationally, four combat vehicles of the Tor-M1
AD missile system enter into the complement of an air
defense missile battery, which is the smallest tactical
element able to independently execute combat
missions. To control the battle performance of the
combat vehicles, the 9S737 Ranzhir automated battery
command post is allocated for the battery.
The manufacturers of the Tor-M1 system render a full
package of maintenance services to keep the system in
combat readiness and offer modernization packages
that markedly expand the system’s combat capabilities.
There are several modifications of the Tor-M1 system,
such as the Tor-M1T (wheeled chassis mounted sys-
tem) and a stationary version.
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q 0,6 - 0,95
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Basic Characteristics
Number of targets:
simultaneously detected 48
simultaneously tracked 2
Target detection range, km 27
Target engagement envelope, km:
range 1.0 - 12.0
altitude 0.01 - 6.0
cross-range 6.0
Target speed, m/s 0 - 700
Minimum target ERA, m
2
-0.1
Response time
(from target detection to missile liftoff), s 4 - 10
Number of missiles on combat vehicle 8
Kill probability:
aircraft 0.6 - 0.95
helicopters 0.8 - 0.96
high-precision weapons 0.6 - 0.95
remotely piloted vehicles 0.6 - 0.98
Maximum vehicle speed, km/h 65
Weight of combat vehicle, kg 37,000
Fuel endurance
(including equipment operation for 2 h), km 500
598
PART 4 4
SHORT-RANGE
AIR DEFENSE MISSILE
AND GUN-MISSILE SYSTEMS
- !"# $ %&
$%' (%)&
GROUP 14 GUIDED MISSILES
Class 1410 Guided Missile
Systems, Complete
14
( ")
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599
PART 4 4
SHORT-RANGE
AIR DEFENSE MISSILE
AND GUN-MISSILE SYSTEMS
- !" #$%
#$& '$(%
GROUP 14 GUIDED MISSILES
Class 1410 Guided Missile
Systems, Complete
14
( ")
:;<< 1410 ;=>?@A> B =C<DBE><=B> <B<?>DA (=CDG:>=<A)
PANTSYR-S1
AIR DEFENSE MISSILE-GUN SYSTEM
Intended to protect troop units and large troop forma-
tions, strategically vital military and industrial facilities
from all types of air attack weapons within a full range
of their combat employment.
System features:
- combined missile-gun armament enabling it to create
an effective zone of solid fire;
- small-size air defense missile featuring high ballistic
characteristics (Vmax = 1,300 m/s) and high fire pow-
er of its fragmentation-rod warhead (the warhead
weighs 20 kg with the sustainer weight of 30 kg);
- absolute jammimg immunity achieved by the use of a
common multimode and multispectral radar/optronic
control system operating in decimetric, centimetric,
millimetric and infrared wave bands;
- capability of firing both guns and missiles on the
move;
- universal nature of target engagement, i.e., engage-
ment of a wide array of aerial targets: aircraft and heli-
copters, small-size guided missiles, guided aerial
bombs, as well as lightly armored ground targets and
manpower;
- fully automatic battle performance, both indepen-
dently or as part of a unit comprising several combat
vehicles;
- high target engagement capability owing to a short
23 -43 "
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600
PART 4 4
SHORT-RANGE
AIR DEFENSE MISSILE
AND GUN-MISSILE SYSTEMS
- !" #$%
#$& '$(%
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reaction time, high speed of air defense missile flight
and availabilty of two independent guidance channels
operating in a wide sector (90° x 90° in azimuth and ele-
vation);
- autonomous combat employment owing to the avail-
abilty of target detection, tracking and engagement
assets in one combat vehicle;
- passive operation mode and extreme accuracy of
guidance owing to the use of a long-wave band infrared
channel with logical signal processing and automatic
target tracking.
The system components are:
- combat vehicle (up to six combat vehicles in one
battery);
- air defense missile;
- gun armament;
- technical support facilities;
- training assets.
The combat vehicle has two types of armament (mis-
siles and guns) and a common multimode and multi-
spectral radar/optronic control system. It comprises a
turret mount to house the armament, laying drives, tar-
get detection and tracking system racks and control
equipment panels. A modular design of the combat
vehicle makes it possible to mount the system on vari-
ous platforms - tracked and wheeled chassis and in
shelters (shelter version of the system) and develop its
simplified versions: a combat vehicle equipped only
with the optronic control system and a combat vehicle
carrying only missile armament.
GROUP 14 GUIDED MISSILES
Class 1410 Guided Missile
Systems, Complete
14
( ")
:;<< 1410 ;=>?@A> B =C<DBE><=B> <B<?>DA (=CDG:>=<A)
601
PART 4 4
SHORT-RANGE
AIR DEFENSE MISSILE
AND GUN-MISSILE SYSTEMS
- !" #$%
#$& '$(%
GROUP 14 GUIDED MISSILES
Class 1410 Guided Missile
Systems, Complete
14
( ")
:;<< 1410 ;=>?@A> B =C<DBE><=B> <B<?>DA (=CDG:>=<A)
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The air defense missile features a two-stage config-
uration with a bicaliber body comprising a separable
booster and a sustainer. The sustainer consists of a
warhead, contact and proximity fuzes, and onboard
equipment.
The gun armament is intended to defeat aerial and
ground targets, as well as enemy manpower. It com-
prises:
- two 2A38M automatic guns;
- ammunition load of 1,400 30mm rounds.
P=0.70 - 0.95
F-16A,
A-10A
P=0.70 - 0.95
Tomahawk
ALCM
F117A,
F22
P=0.85 - 0.95
602
PART 4 4
SHORT-RANGE
AIR DEFENSE MISSILE
AND GUN-MISSILE SYSTEMS
- !" #$%
#$& '$(%
Basic Characteristics
Armament AD missiles and guns
Ammunition load, pc:
air defense missiles on launchers 8 - 12 (depending on chassis type)
30mm rounds 1,400
Fire control system components TAR, TMTR (mm+cm wave bands),
IR direction finder, thermal imager
Range, km:
target detection 36 - 38
target tracking 24 - 30
Target engagement envelope, m:
missiles:
range 1,000 - 18,000
altitude 5 - 10,000
gun:
range 200 - 4,000
altitude 0 - 3,000
Maximum target speed, m/s 1,000
Missile guidance radio commands with IR
and radio direction finding
Number of simultaneously
engaged targets 2 (in sector measuring 90° x 90°
in azimuth and elevation)
Reaction time, s 4 - 6
Missile salvo fire capability ensured
Ground target engagement capability ensured
Crew 3
Service life, years 25
Maximum missile speed, m/s 1,300
Missile weight, kg:
in transport-launch canister 85
launch weight 71
Missile length in canister, mm 3,200
Missile caliber, mm:
booster 170
sustainer 90
Warhead:
weight, kg 20
fuze type contact + proximity,
radar-controlled, adaptive
Type of gun armament 2A38M (two twin-barreled automatic guns)
Caliber, mm 30
Types of projectiles HE fragmentation, fragmentation tracer
Muzzle velocity, m/s 970
Barrel life, rds 8,000
GROUP 14 GUIDED MISSILES
Class 1410 Guided Missile
Systems, Complete
14
( ")
:;<< 1410 ;=>?@A> B =C<DBE><=B> <B<?>DA (=CDG:>=<A)
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603
PART 4 4
SHORT-RANGE
AIR DEFENSE MISSILE
AND GUN-MISSILE SYSTEMS
- !"# $ %&
$%' (%)&
GROUP 14 GUIDED MISSILES
Class 1410 Guided Missile
Systems, Complete
14
( ")
:;<< 1410 ;=>?@A> B =C<DBE><=B> <B<?>DA (=CDG:>=<A)
OSA-AKM AUTONOMOUS ALL-WEATHER
CLOSE-IN GROUND FORCES
AIR DEFENSE MISSILE SYSTEM
Intended for defense of troops on the march and in
mobile combat, as well as strategic ground facilities
against air strikes delivered by piloted and pilotless air
vehicles flying at low and medium altitudes.
The Osa-AKM system components are:
Combat assets
The 9A33BM3 (9A33BM2) combat vehicle.
The combat vehicle is mounted on a self-propelled
amphibious wheeled chassis. It is an autonomous
mobile combat vehicle, which can detect aerial targets
while stationary or on the move, automatically track and
engage them. To defeat a target, the combat vehicle
opens fire from a short halt. High-priority targets can
be engaged by a two-missile salvo.
The combat vehicle comprises:
- self-propelled wheeled chassis;
- target acquisition radar with an IFF radar interrogator;
- target tracking radar;
- two-channel missile aiming radar;
- two-channel command transmitter;
- computer;
- TV-optical sight;
- primary power supply system;
- radio communications system.
The 9M33M3 (9M33M1) air defense missile.
The missile features a canard aerodynamic configura-
tion and is provided with a transport launch canister. A
solid-propellant two-mode rocket motor imparts the
flight speed to the missile enabling it to engage high-
speed and maneuvering targets. The missile is provid-
ed with a high-explosive fragmentation warhead with a
delayed fuze action depending on the missile-to-target
closing rate and the type of target to achieve the max-
imum kill efficiency.
3 4 3434 354
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- _ckg=;@;:p@;a <?;@qBa G>^>_;EB =CD;@_ @; ^;=>?A;
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- <B<?>D; G>^cBE@CiC r:>=?^CGB?;@Ba;
- <B<?>D; ^;_BC<ca`B.
- >@B?@;a kG^;c:a>D;a ^;=>?; 9$33$3 (9$33$1).
;=>?; =CDG:>=<; cAGC:@>@; GC ;r^C_B@;DBE><=Cd <g>D> «k?=;».
s^;@>@B>, ?^;@<GC^?B^Cc=; B >> <?;^? Ch><G>EBc;o?<a ?^;@<-
GC^?@C-Gk<=CcAD =C@?>d@>^CD. c>^_C?CG:Bc@Ad _ckg^>fBD@Ad
_cBi;?>:p G^B_;>? ^;=>?> r@>^iCcCC^kf>@@C<?p, @>ChgC_BDko
_:a GC^;f>@Ba <=C^C<?@Ag B D;@>c^B^kobBg q>:>d. nC>c;a
E;<?p C<=C:CE@C-tki;<@CiC _>d<?cBa, GC_^Ac >> C<kb><?c:a>?<a
< `;_>^f=Cd, `;cB<ab>d C? <=C^C<?B <h:Bf>@Ba ^;=>?A < q>:po
B ?BG; q>:B _:a GC:kE>@Ba D;=<BD;:p@Cd rtt>=?Bc@C<?B GC^;-
f>@Ba.
Technical support assets:
- 9T217BM2 transporter-loader;
- 9V914 survey vehicle;
- 9V242-1 mobile automated test station;
- 9V210M3 maintenance vehicle;
- 9F632 operator training simulator;
- 9F372M3 SPTA set;
- 9F16M2 ground equipment kit.
Manufacturers render a full package of maintenance
services to keep the system in combat readiness, as
well as packages of modernization to enhance the sys-
tem combat capabilities.
The Osa-AKM system can also be modified for use in
the Saman target missile system.
=NOPQ=@RP= @A=B@C>D:
- ?^;@<GC^?@C-`;^af;ob;a D;eB@; 9217n$2;
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- ;c?CD;?B`B^Cc;@@;a =C@?^C:p@C-B<GA?;?>:p@;a GC_cBf@;a
<?;@qBa 9w242-1;
- D;eB@; ?>g@BE><=CiC Ch<:kfBc;@Ba 9w210$3;
- ?^>@;f>^ CG>^;?C^Cc 9x632;
- 9x372$3.
- =CDG:>=? @;`>D@CiC ChC^k_Cc;@Ba 9x16$2.
^>_G^Ba?Ba-B`iC?CcB?>:B C=;`Ac;o? GC:@Ad =CDG:>=< <>^cB<-
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@O<>O?= NDADRC=AP@CPRP
(;:p@C<?p Ch@;^kf>@Ba q>:>d (?BGCcCiC <;DC:>?; ), =D 45
z^;@BqA `C@A GC^;f>@Ba:
GC _;:p@C<?B, =D 1,5 - 10
GC =k^<CcCDk G;^;D>?^k, D _C 6000
&=C^C<?p GC^;f;>DAg q>:>d, D/< 10 - 500
$;@>c^ q>:B, >_. _C 8
w^>Da:
^>;=qBB, < 18 - 26
G>^>cC_; B` GCgC_@CiC GC:Cf>@Ba c hC>cC>, DB@. _C 4
G>^>`;^af;@Ba !, DB@. 5
$;<<; ^;=>?A, =i:
<?;^?Cc;a 127
hC>cCd E;<?B 15
C:BE><?cC ^;=>? @; ! 6
w>^Ca?@C<?p GC^;f>@Ba:
?BGCcCd @>D;@>c^B^kob>d q>:B 0,4 - 0,96
c>^?C:>?Cc 0,24 - 0,76
&=C^C<?p G>^>_cBf>@Ba n$, =D/E:
GC eC<<>d@AD _C^Ci;D 60
GC i^k@?CcAD _C^Ci;D 30
GC h>`_C^Cfpo 10
@; G:;ck 8
;G;< gC_; n$ GC ?CG:Bck
(G^B _ckgE;<CcCd ^;hC?> ;GG;^;?k^A), =D 250
Basic Characteristics
Target (typical tactical aircraft) detection range, km 45
Target engagement envelope:
range, km 1.5 - 10
cross-range, m up to 6,000
Target speed, m/s 10 - 500
Target g-load, g up to 8
Time of:
reaction, s 18 - 26
deployment from march, min up to 4
launcher reloading, min 5
Missile weight, kg:
at launch 127
warhead 15
Number of missiles on launcher 6
Kill probability:
typical nonmaneuvering target 0.4 - 0.96
helicopters 0.24 - 0.76
Combat vehicle speed, km/h:
on highway 60
on dirt road 30
cross-country 10
in water 8
Combat vehicle fuel endurance
(including equipment operation for 2 h), km 250
604
PART 4 4
SHORT-RANGE
AIR DEFENSE MISSILE
AND GUN-MISSILE SYSTEMS
- !"# $ %&
$%' (%)&
GROUP 14 GUIDED MISSILES
Class 1410 Guided Missile
Systems, Complete
14
( ")
:;<< 1410 ;=>?@A> B =C<DBE><=B> <B<?>DA (=CDG:>=<A)
605
PART 4 4
SHORT-RANGE
AIR DEFENSE MISSILE
AND GUN-MISSILE SYSTEMS
- !"# $ %&
$%' (%)&
2K22M1 TUNGUSKA-M1
AIR DEFENSE GUN-MISSILE SYSTEM
Intended to protect tank and motorized rifle units of the
Ground Forces in all forms of combat and small-size
objects from air attack weapons, primarily fire-support
helicopters, and defeat lightly armored ground and sur-
face targets.
The system features:
- combined missile-gun armament enabling it to create
an effective zone of solid fire;
- high autonomous combat capability due to the avail-
abilty of target detection and tracking radars on a sin-
gle combat vehicle;
- ability to carry out airspace circular radar scanning
while stationary and on the move;
- capability of both successive and separate fire deliv-
ered by the missile and gun armament at aerial target-
s;
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U RXPOKFU]O` TOJOERTIHOF` bFLO
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Basic Characteristics
Types of engaged targets helicopters, aircraft, cruise missiles,
ground and waterborne targets
Range, km:
target detection up to 18
target tracking up to 16
Maximum target speed, m/s 500
Target engagement envelope, m:
gun armament:
altitude from 0 to 3,000
range from 200 to 4,000
missile armament:
altitude from 15 to 3,500
range from 2,500 to 10,000
Gun armament performance:
gun number, type and caliber 2 x 2A38M x 30mm
muzzle velocity, m/s 960
rate of fire of two guns, rds/min up to 5,000
Missile armament performance:
maximum missile speed, m/s 900
warhead high-explosive fragmentation, rod-type
warhead weight, kg 9
warhead effective radius, m up to 5
guidance system semiautomatic, radio-command,
with optical sighting of target
Kill probability:
gun armament 0.24 - 0.6
missile armament 0.5 - 0.65
Time of:
reaction, s 8 - 10
deployment from march, min up to 5
full reloading with aid of transloader, min up to 16
Combat vehicle weight, t 34
Crew 4
606
PART 4 4
SHORT-RANGE
AIR DEFENSE MISSILE
AND GUN-MISSILE SYSTEMS
- !"# $ %&
$%' (%)&
- ability to fire automatic guns while the combat vehicle
is stationary or on the move, day and night, in any
weather conditions and launch missiles while stationary
or from a short halt in visual target environment.
The system comprises:
- 2S6M1 combat vehicles;
- 9M311-3M air defense missiles;
- 30mm rounds;
- 9F77M transporter-
loaders;
- 9F55-1M1 repair and
maintenance vehicle;
- 1R10-1M1 repair and
maintenance vehicle;
- MTO-AGZ (ATG) main-
tenance vehicle;
- 9V921-M automated
test station.
The battle performance
of the air defense bat-
tery, incorporating six
combat vehicles, is con-
trolled by the Ranzhir
unified command post.
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GROUP 14 GUIDED MISSILES
Class 1410 Guided Missile
Systems, Complete
50-,, 14 01'(*' ) 1/2)'1)'
)'2* (1/2,3'1*)
LIUU 1410 I]FPHQF O ]RU`OKFU]OF UOUPF`Q (]R`XLF]UQ)
607
PART 4. 4.
CLOSE-IN AIR DEFENSE
WEAPON SYSTEMS
!
"!#$
% &' ()!$*
GROUP 14 GUIDED MISSILES
Class 1410 Guided Missile
Systems, Complete
14 !
! ( !#)
;<== 1410 ><?@ABC@ D ?E=FDG@=?D@ =D=A@FC (?EFI;@?=C)
SOSNA AIR DEFENSE GUN-MISSILE SYSTEM
Intended to defeat tactical aircraft and helicopters,
cruise missiles, remotely piloted vehicles, as well as
lightly armored ground targets. The Sosna-A air
defense artillery system is its modified version.
The system features:
- high fire power due to the combination of the missiles
and 30mm 2F38 twin-barreled air defense automatic
gun;
- high effectiveness against high-speed targets and heli-
copters, including those performing a pop-up maneuver,
ensured by a laser-guided hypersonic missile;
- high effectiveness of target engagement by the gun
due to high accuracy of target tracking, lead angle
computation and followup;
- automated battle performance due to optronic target
detection and automatic tracking system, digital com-
puter for computation of launch zones and lead angles,
and electric power drives;
- day and night employment capability due to the use
of a thermal imaging channel in the optronic target
detection and automatic tracking system;
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