-
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MISSILE AND GUN ARMAMENT
ISKANDER-E
THEATER MISSILE SYSTEM
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The system is intended to use conventional warheads
for engagement of pinpoint and area targets, such as:
- hostile fire weapons (missile systems, multiple launch
rocket systems, long-range artillery pieces);
- air and antimissile defense weapons;
- fixed- and rotary-wing aircraft at airfields;
- command posts and communications nodes;
- critical civilian infrastructure facilities;
- other vital pinpoint and area targets.
The missile system ensures:
- high probability of fire mission accomplishment in
hostile active countermeasures environments;
- high probability of failure-proof functioning of the missile during its launch preparation and in flight;
- automatic computation and input of missile flight missions by the launcher devices;
- high tactical maneuverability and strategic mobility
owing to transportability of the system vehicles by all
types of transport;
- automation of battle management of missile units and
their information support;
- long service life and ease of operation.
The Iskander-E system is equipped with a solid-propellant single-stage guided missile controlled throughout
the entire flight path and provided with a nonseparable
warhead.
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Scheduled inspection
and maintenance vehicle
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Command and staff vehicle
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Data preparation station
Basic Characteristics
Launch range, km:
maximum
minimum
Weight, kg:
missile launch
payload
launcher
Warhead
Guidance system
Chassis
Number of missiles:
on launcher
on transloader
Time to launch, min:
from highest readiness state
after march
Assigned service life, yr
Crew
Operating temperature range, °C
GROUP 10 WEAPONS
Class 1055 Launchers, Rocket
and Pyrotechnic
2
2
31 ?4-11 4
31 ?4-11 16
10
3
±50
10
-.// 1055
.012341 5446781391
83
PART 1
MISSILE SYSTEMS
1
TOCHKA-U MODERNIZED
TACTICAL MISSILE SYSTEM
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The system is designed to effectively defeat critical targets in the tactical depth of the enemy battle formation.
Components:
- solid-propellant missiles with submunition warhead
and with HEF warhead;
- self-propelled launcher (SPL);
- transloader;
- transporter;
- automated test vehicle;
- maintenance vehicle;
- arsenal equipment set;
- missile and warhead containers.
The single-stage solid-propellant missile with an inseparable warhead is inertially controlled throughout its flight
path.
The self-propelled launcher determines the coordinates
of its location, performs the prelaunch preparation and
laying of a missile, computes the flight mission data
and launches the missile from a deployed fire position
with the crew staying in the cabin.
The transloader is designed to carry missiles, perform
loading and unloading operations and to mate warheads to missiles.
The warhead is designed for ballistic
battlefield and theater missiles.
Components: optical homing head,
inertial unit, onboard computers,
onboard automatic control devices,
electrohydraulic or electric control actuators.
HYDRAULIC DRIVES
AND THEIR ELEMENTS
FOR SELF-PROPELLED
MISSILE LAUNCHERS
10 - 20
15 - 20
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The drives are designed to perform
the following operations in the automatic mode:
- jacking and leveling of SPLs on
organized and deployed sites;
- elevation of guides to an assigned
angle and their retention in position during the preparation and execution of a combat mission;
- opening of covers and hatch doors and locking of
mechanisms in the traveling position;
- control of movement of armor and automotive pieces.
Electrohydraulic control actuators
Motion of output member of actuators:
translatory, mm
rotary, deg
Time of full stroke of output member, s
Output member shaft power, kW
Accuracy of driving to desired position, %
Electric control actuators
Range of control surface rotation, deg
Maximum rate of control surface rotation, deg/s
Control surface pivot pin torque, N.m
Band of reproduced frequencies, Hz
up to 200
±30
up to 0.1
up to 10
1 or better
±30
130
30
40
INFORMATION SUPPORT
AND AUTOMATED BATTLE MANAGEMENT
OF MISSILE FORMATIONS
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The backbone of the system is unified target designation vehicles (TDV) and command and staff vehicles
(CSV) that operate in the automated
mode and ensure the reception and
processing of video and formalized
intelligence data, generation of coordinate and reference target designation, distribution of targets, solution
of optimization problems during the
preparation of proposals for making
battle management decisions and
transmission of decisions and requisite information to missile launchers.
GROUP 10 WEAPONS
Class 1055 Launchers, Rocket
and Pyrotechnic
10
-.// 1055
.012341 5446781391
86
PART 1
MISSILE SYSTEMS
Basic Characteristics
Base vehicle
Power supply system
Automated work stations
Personal computers
Local computer network
Electronic cartography
Radio set
Number of communications channels
Accuracy of determining
own coordinates, m
command signals, manual
or semiautomatic, wire-guided
Firing range, m
400 - 3,000
Weight, kg
12.5
Mean fight speed, m/s
130
Caliber, mm
125
Length with HE warhead, mm
860
Length with HEAT warhead (in combat configuration), mm
1,005
Warhead weight (HEAT, HE), kg
3.5
HEAT warhead armor penetration, mm
800
GROUP 14 GUIDED MISSILES
Class 1425 Guided Missile
Systems, Complete
14
0122 1425 34506728 95:1;0?8= 2@2>64
91
PART 1
ANTITANK GUIDED MISSILE
SYSTEMS
1
KONKURS-M
ANTITANK GUIDED MISSILE SYSTEM
/ 0/ 1 / 2
1 2 /
The system is designed to engage modern armor
materiel provided with explosive reactive armor (ERA),
fortified weapon emplacements, mobile and stationary
pinpoint ground and waterborne targets, low flying helicopters and other targets, both day and night, in
adverse weather conditions.
The system comprises the 9P135M1 launcher,
9M113M guided missiles, the 1PN79-2 thermal sight
and test equipment for the launcher, missiles and sight.
The system is mounted on the 9P148 combat vehicle.
The system can be pintle-mounted (without tripod) on
wheeled and tracked combat vehicles (BMP, BMD,
BTRD, MT-LB), jeep-type light carriers, and other transport facilities.
If the need arises, the launcher and missiles can be
rapidly removed from the vehicle together with the thermal sight and remotely emplaced for independent fire.
The ammunition comprises 9M111 (9M111M) and
9M113 missiles of the Fagot and Konkurs systems.
Irrespective of missiles used, the operator’s actions
remain the same.
To train operators in a classroom, provision is made for
the 9F660-3 computer-aided trainer and a set of instructional missiles (full-scale mockup, sectionalized missile
and functioning onboard
equipment model).
Warhead
Armor penetration, mm
ERA penetration
Firing range, m:
by day
by night
Guidance
Weight, kg:
launcher
container with missile
Overall dimensions, mm:
length of container with missile
missile caliber
Operating temperature range, °C
Crew
75 - 4,000
75 - 3,500
semiautomatic with commands
transmitted over wire link
22
26.5
1,263
135
±50
2
GROUP 14 GUIDED MISSILES
Class 1425 Guided Missile
Systems, Complete
14
0122 1425 34506728 95:1;0?8= 2@2>64
92
PART 1
ANTITANK GUIDED MISSILE
SYSTEMS
1
KORNET-E
ANTITANK GUIDED MISSILE SYSTEM
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The system is intended to defeat current and future
tanks provided with explosive reactive armor, lightly
armored targets, fortifications (bunker and log
emplacements) and low flying air targets (hovering
helicopters).
The system components:
- launcher with a tracker, laying drives and a missile
launch mechanism;
- thermal sight;
- guided missiles kept in launching transporting containers.
The missiles are fitted with two types of warheads: the
tandem HEAT warhead and the thermobaric warhead
possessing the high-explosive and incendiary effect of
a large-caliber artillery projectile.
The small weight and dimensions of the launcher, the
night sight and missiles make it possible to use the
Kornet-E system independently or install it on various
wheeled and tracked combat vehicles, including the
BMP-3 ICV with an automated ammunition stowage
rack.
It is possible to fire two missiles at one target simultaneously.
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Basic Characteristics
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Armor penetration
Firing range, m:
by day
by night with the use of thermal sight
Guidance system
Weight, kg:
portable launcher
thermal sight
ATGM
Laying angles, deg:
azimuth
elevation
Operating temperature range, °C:
usual conditions
hot desert climate
Crew
defeat
of ERA-provided
current and future tanks
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The system is designed to defeat modern armored targets, weapon emplacements and other pinpoint targets, and can also be used by special-designate units
for urban and antiterrorist fighting.
The system components: launcher, containerized missiles and test equipment for the launcher.
The system allows delivery of fire in the prone position
from organized and deployed sites, firing from the
standing foxhole position as well as firing from the
shoulder and carrying the ATGM system in packs, with
pack No. 1 containing the launcher and missile in the
firing attitude and pack No. 2 accommodating three
Metis missiles.
Organizational and field maintenance of the ATGM system is carried out with the help of test equipment.
To train operators, use is made of field and computeraided trainers.
Warhead
Armor penetration, mm
Firing range, m:
maximum
minimum
Guidance
Time into and out of action, s
Rate of fire, rds/min
Weight, kg:
launcher
container with missile
Overall dimensions, mm:
missile caliber
container length
Weight of packs, kg:
№ 1 (launcher and missile)
№ 2 (three missiles)
The system is designed to defeat armored targets, fortifications and weapon emplacements.
The system components: launcher, containerized missiles, thermal sight and test equipment for the launcher and thermal sight.
The missiles are fitted with warheads of two types: a
tandem HEAT warhead and a thermobaric warhead
possessing the high-explosive and incendiary effect of
the 155mm artillery projectile.
The system allows delivery of fire in the prone position
from organized and deployed sites, firing from the
standing foxhole position as well from the shoulder,
and carrying the ATGM system in packs, with pack No.
1 containing the launcher and missile in the firing attitude and pack No. 2 accommodating two Metis-M missiles.
Organizational and field maintenance of the ATGM system is carried out using test equipment.
To train operators, use is made of field and computeraided trainers.
