Каталог - Оружие России 2000 c82-795

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412

PART 2  2

ANTITANK

GUIDED MISSILES



 

SHTURM ANTITANK

GUIDED MISSILE

The missile is designed to engage moving and fixed

pinpoint armored ground targets, as well as slow flying

air targets.

The missile is a complete round comprising three com-

ponents: missile proper, booster, and launch tube

which also serves as a container. It is of the canard

configuration and mounts folding control surfaces (one

pair) and four folding arc-shaped wings.

The single-channel semiautomatic radio command con-

trol system ensures matching-curve guidance. In flight,

the missile rotates about its longitudinal axis. The radio

equipment has a high jamming immunity, owing to the

switching of five letter frequencies and two remotely

controlled codes, which allows simultaneous attack of

closely located targets by ten helicopters. In addition, a

narrow antenna radiation pattern and comparatively

short radiation cycle hampers enemy jamming.

Missile coordinates are measured relative to the target

sight line by the direction finder of the Raduga equip-

ment installed on the Mi-24V parent helicopter. The

field of view of the direction finder is nine degrees in

the lockon channel and two degrees in the tracking

channel. The coordinates measured by the direction

finder are fed to the unit to shape command signals

sent to the radio link equipment and emitted in the

direction of the missiles as SHF pulse trains via the

movable antenna system. The control equipment

receives these pulses and transforms them into IR



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FUS PMHEQZFUS [DJD\.

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(IDXUCD LDCG).

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GROUP 14

GUIDED MISSILES

Class 1410 Guided Missiles

) 14 !*!  "!!

!"* (" !*)

JGTT 1410 LCGPJKDVUD CGYDXU O CGYDXU-FMTOXDJO

413

PART 2  2

ANTITANK

GUIDED MISSILES



 

responder signals and steering yaw and pitch com-

mands applied to the missile actuator.

The launch tube serves as a guide for the fired missile

and also as a container for missile transportation, stor-

age and carriage.

Carrier: Mi-24V.

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CMV LCO XCGFTLMCXOCMPYD, SCGFDFOO O LDCDFMTYD CGYDXU.

MTOXDJb: O-24.

-./0.12 345467258-7868

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WMDPM\ IGTXO 5,4

kMDPGK IGTXb YQVQJKXOPFM-MTYMJMIFGK, lh

kCMFDLCMWOPGDVMTXb, VV 650

hOTXDVG FGPDEDFOK CGEOMYMVGFEFGK

DCMKXFMTXb LMLGEGFOK P XGFY 0,65 - 0,9

hCDEFKK TYMCMTXb LMJDXG, V/T 420

oGWGCOXFUD CGHVDCU FGLCGPJK]RD^M QTXCM\TXPG

(EJOFG S PUTMXG S ZOCOFG), V 1,98 S 0,37 S 0,33

Basic Characteristics

Max launch range, km 5

Launch weight, kg 35

Warhead weight, kg 5.4

Warhead type HEAT fragmentation, FAE

Armor penetration, mm 650

Guidance system radio command

Tank hit probability 0.65 - 0.9

Average flight speed, m/s 420

Overall dimensions

of container

(length S height S width), m 1.98 S 0.37 S 0.33

GROUP 14

GUIDED MISSILES

Class 1410 Guided Missiles

) 14 !*!  "!!

!"* (" !*)

JGTT 1410 LCGPJKDVUD CGYDXU O CGYDXU-FMTOXDJO

GROUP 14

GUIDED MISSILES

Class 1410 Guided Missiles

) 14 !*!  "!!

!"* (" !*)

JGTT 1410 LCGPJKDVUD CGYDXU O CGYDXU-FMTOXDJO

414

PART 2  2

ANTITANK

GUIDED MISSILES



 

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!!, /:

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61)'*&)!*% +)+(&"' 2 *& 0,65 - 0,9

=16(&'' ! )1)!*% +)$6*, #/! 400

Basic Characteristics

Max launch range, km 6

Launch weight, kg 42.5

Warhead weight, kg 7.4

Warhead type HEAT, rod, FAE

Armor penetration (with ERA), mm 800

Guidance system radio command

Tank hit probability 0.65 - 0.9

Average flight speed, m/s 400

ATAKA ANTITANK GUIDED MISSILE

The missile is designed to engage pinpoint armored

and slow flying air targets, as well as weapon

emplacements of the enemy.

After the helicopter crew decides to launch a missile,

the navigator (operator) aligns the fixed mark with the

target and presses the input button, thereby selecting

the corrected program target tracking mode. As a

result, the laser range finder measures the target

range in the automatic mode and presents the

obtained data on the multifunctional display, as well as

the information on requisite maneuvers to bring the

helicopter to a permissible launch zone. The pilot flies

the helicopter to keep the movable target mark in the

fixed square.

The operator makes sure that the fixed mark is aligned

with the target and, if necessary, makes corrections

by manipulating the guidance unit joysticks. When the

helicopter is in the permissible launch zone, the digi-

tal computer sends the in-range command to the mul-

tifunctional display. On this command the operator

performs missile launch.

During missile flight, the operator keeps the fixed

mark on the multifunctional display in alignment with

the target and, if necessary, adjusts the position of the

sight line by manipulating the guidance unit joysticks

until the impact of the missile with the target. During

this process, the helicopter can maneuver in yaw with-

110 degrees with banks of up to 30 degrees.

The launch tube serves as a guide for the fired missile

and also as a container for missile transportation,

storage and carriage.

Carriers: Mi-24V, Mi-24P, Mi-28.

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GROUP 14

GUIDED MISSILES

Class 1410 Guided Missiles

=.4-- 14 .261>6 / 27/62/6

/67> (27-562>)

$!! 1410 +12$'6#l6 1 6*l " 1 6*l-&)!"*6$"

415

PART 2  2

ANTITANK

GUIDED MISSILES



 

VIKHR SUPERSONIC GUIDED MISSILE

The missile is designed to engage vital ground targets,

including armored targets fitted out with built-in and

add-on explosive reactive armor, at a range of up to 10

km in daytime and up to 5 km at night, as well as air

targets in conditions of air defense assets activity.

The Vikhr missile is part of the Vikhr-M system, which

also includes an automatic sight, an aircraft launcher,

and a 30mm automatic gun.

The automatic sight is provided with TV and IR channels

of target sighting, a laser beam channel of missile con-

trol, a laser rangefinder, an automatic target tracking

unit, a digital computer and a system of stabilization

and aiming of sighting and beam channels. The auto-

matic sight provides for target detection and identifica-

tion both day and night, automatic target tracking and

missile guidance, and generates exact information for

gun and rocket firing.

The guided missile is kept in a sealed launching trans-

porting container and consists of a HEAT fragmentation

warhead fitted with a contact and a proximity fuze, an

air-dynamic control actuator, control electronics, a

motor and a laser detector.

The Vikhr-M system with its supersonic missile having

a launch range of up to 10 km and an automatic target-

tracking system permits the carrier aircraft to leave the

air defense engagement zone after missile launch,

which enhances its combat survivability. The HEAT

fragmentation warhead fitted with a contact and a prox-

imity fuze can engage armored ground and air targets.

The use of the proximity fuze makes it possible to

engage an air target at a near miss of up to 5 m. It

gives the carrier additional advantage for air duels. The

Vikhr missile laser beam control system provides for its

precise guidance owing to data transmission to the

missile in the course of its launch, which is excluded in

homing systems. The Vikhr missile control system has

high jamming immunity because its receiver faces the

carrier, thereby protecting it from jamming signals.

The high pinpoint target hit probability is provided by

 !" #$"%"   «'»

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JAMBRDMQE HEFBADK_K MFH[GBDMI.

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OPNS OPABHNYU CK 10 QR M ETPKREPMGBOQKX OMOPBRKX OHB-

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TUOPABHE TUVKCMPN MF FKDU KYOPABHE, GPK KYBOJBGMTEBP

B_K TULMTEBRKOPN T YKS. [R[HIPMTDK-KOQKHKGDEI YKBTEI

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DMI AEQBPU DE WBHN FE OGBP JBABCEGM MD`KAREWMM DE DBB

T JAKWBOOB J[OQE, GPK MOQHSGBDK T OMOPBREV OERKDETBCB-

GROUP 14

GUIDED MISSILES

Class 1410 Guided Missiles

+## 14  ,- ' !%' '

'%- ( !%#$ -)

HEOO 1410 JAETHIBRUB AEQBPU M AEQBPU-DKOMPBHM

416

PART 2  2

ANTITANK

GUIDED MISSILES



 

the automatic target tracking system and highly accu-

rate missile control system that makes allowance for

changes in the parameters of the carrier and the target

in the course of firing.

Salvo fire is possible by launching two missiles at one

target.

The upgraded system is capable of launching the Vikhr

missiles against two to four targets at a range of 10 km

during 30 s, which increases its fire power potential

three to four times.

The carriers can be modernized during the next sched-

uled overhaul by installing the Vikhr system and partial-

ly updating the electronics and separate systems,

which does not require heavy expenses.

An important feature of the Vikhr-M system is self-

containment and modularity of its control, aiming and

guidance systems enabling modernization of the car-

riers without their considerable updating. All units of

the system are series-produced and feature a high

level of reliability. The Vikhr system requires no main-

tenance throughout its entire service life. The proper-

ties of the Vikhr-M system allow its simple adaptation

to a number of carriers practically without changing

their systems.

The development work involving the Vikhr-M system

arrangement on a carrier can be performed during a

short period (1.5 to 2 years) with low financial expens-

es as compared with acquisition or development of a

new carrier armed with up-to-date weapons.

DMI. iMOPBRE [JAETHBDMI AEQBPKX «MVAN» KYHECEBP TUOK-

QKX JKRBVK[OPKXGMTKOPNS YHE_KCEAI PKR[, GPK JAMBRDMQ

MFH[GBDMI KYAEZBD T OPKAKD[ DKOMPBHI M DE B_K TVKC MO-

QHSGBDK JKJECEDMB KA_EDMFKTEDDUV JKRBV.

UOKQEI TBAKIPDKOPN JKJECEDMI T REHKAEFRBAD[S WBHN

CKOPM_EBPOI FE OGBP ETPKREPMGBOQKX OMOPBRU OHBLBDMI FE

WBHNS M TUOKQKPKGDKX OMOPBRU [JAETHBDMI AEQBPKX, [GM-

PUTESZBX MFRBDBDMB JEAERBPAKT DKOMPBHI M WBHM T JAK-

WBOOB OPABHNYU.

KFRKLDE FEHJKTEI OPABHNYE CT[RI AEQBPERM JK KCDKX WBHM.

KCBADMFMAKTEDDUX QKRJHBQO OJKOKYBD TBOPM FEHJKT[S

OPABHNY[ AEQBPERM «MVAN» JK CT[R - GBPUABR WBHIR DE

CEHNDKOPM 10 QR FE 30 O, GPK JKTU\EBP B_K YKBT[S JAKMF-

TKCMPBHNDKOPN T 3 - 4 AEFE.

KCBADMFEWMI DKOMPBHBX TKFRKLDE JAM KGBABCDKR JHE-

DKTKR ABRKDPB J[PBR AEFRBZBDMI QKRJHBQOE «MVAN» M

GEOPMGDKX CKAEYKPQM AECMKaHBQPAKDDK_K KYKA[CKTEDMI M

KPCBHNDUV OMOPBR, GPK PABY[BP DBFDEGMPBHNDUV REPBAM-

EHNDUV FEPAEP.

ELDEI KOKYBDDKOPN QKRJHBQOE «MVAN-» - ETPKDKRDKOPN

M RKC[HNDKOPN OMOPBR [JAETHBDMI, JAMWBHMTEDMI M DETB-

CBDMI, GPK JKFTKHIBP JAKTKCMPN RKCBADMFEWMS DKOMPBHBX

YBF FDEGMPBHNDKX CKAEYKPQM. OB YHKQM QKRJHBQOE MF_KPE-

THMTESPOI OBAMXDK M MRBSP TUOKQMX [AKTBDN DECBLDKOPM.

«MVAN» DB PABY[BP PBVDMGBOQK_K KYOH[LMTEDMI T PBGBDMB

TOB_K OAKQE aQOJH[EPEWMM. iTKXOPTE QKRJHBQOE «MVAN-»

JKFTKHISP HB_QK ECEJPMAKTEPN B_K Q WBHKR[ AIC[ DKOMPB-

HBX JAEQPMGBOQM YBF CKAEYKPQM MV OMOPBR.

JUPDK-QKDOPA[QPKAOQEI AEYKPE JK AEFRBZBDMS QKRJ-

HBQOE «MVAN-» DE DKOMPBHB RKLBP YUPN TUJKHDBDE T QK-

AKPQMX OAKQ (1,5 - 2 _KCE) O DBYKHN\MRM `MDEDOKTURM FE-

PAEPERM JK OAETDBDMS O FEQ[JQKX MHM AEFAEYKPQKX DKTK-

_K DKOMPBHI O OKTABRBDDUR TKKA[LBDMBR.

!0123145 67879:58;0:;9;

jEHNDKOPN OPABHNYU, R 10000

EOOE AEQBPU, Q_ 45

KHBPDKB TABRI JAM CEHNDKOPM 5000/8000 R, O 11/21

BAKIPDKOPN JKJECEDMI T WBHN PMJE «PEDQ» 0,8 - 0,9

nKBTEI GEOPN Q[R[HIPMTDK-KOQKHKGDK-

`[_EODEI PEDCBRDK_K PMJE

MJ TFAUTEPBHI QKDPEQPDUX M DBQKDPEQPDUX

nAKDBJAKYMTEBRKOPN

FE CMDERMGBOQKX FEZMPKX, RR 1000

iMOPBRE:

OKJAKTKLCBDMI WBHM ETPKREPMGBOQEI

[JAETHBDMI AEQBPKX HEFBADK-H[GBTEI

Basic Characteristics

Launch range, m 10,000

Missile weight, kg 45

Flight time at 5,000/8,000 m range, s 11/21

Tank-type target hit probability 0.8 - 0.9

Warhead type tandem HEAT

fragmentation

Fuze type contact

and proximity

Armor penetration behind ERA, mm 1,000

Target-tracking system automatic

Missile guidance system laser beam

GROUP 14

GUIDED MISSILES

Class 1410 Guided Missiles

+## 14  ,- ' !%' '

'%- ( !%#$ -)

HEOO 1410 JAETHIBRUB AEQBPU M AEQBPU-DKOMPBHM

PART 2  2

GROUP 13 AMMUNITION

AND EXPLOSIVES

Class 1325 Bombs

 13  !",  $" ! % 

! $&"$" $ ' $

 1325  

417

AIR BOMBS $%&%'(()* +',+)

( $)* + $!,!(( $- (!

UNGUIDED AIRCRAFT ARMAMENT

OFAB-100-120 HIGH EXPLOSIVE

FRAGMENTATION BOMB

This bomb is designed to engage lightly armored and

easily vulnerable materiel, military industrial facilities,

as well as manpower. It is dropped from altitudes of

500 to 15,000 m at a speed of 500 to 1,150 km/h.

%)(-4(* $!,!((*

+ 4-100-120

BCDEF DG HCIG JKCCL 

JKMGEL NOK, -HCQO RKN

 IL . BCGNG  N 500 - 15000  HC

KCNGO 500 - 1500 K/F.

567869: ;<=<>?:=@5?@>@

SNC,  273

S (E ECNG),  1065

,, KJ:

 123

$$ 46 (XY)

Basic Characteristics

Diameter, mm 273

Length (without fuze), mm 1,065

Weight, kg:

bomb 123

explosive 46 (XE)

OFAB-250-270 HIGH EXPLOSIVE

FRAGMENTATION BOMB

This bomb is designed to engage military industrial

facilities, lightly armored and easily vulnerable materiel

as well as manpower.

It is dropped from altitudes of 500 to 16,000 m at a

speed of 500 to 1,500 km/h.

%)(-4(*

$!,!((* + 4-250-270

BCDEF DG HCIG -HCQO

RKN, JKCCL  JKMGEL NOK,

IL .

BCGNG  N 500 - 16000  HC KCNGO 500 -

1500 K/F.

567869: ;<=<>?:=@5?@>@

SNC,  325

S,  1456

,, KJ:

 266

$$ 94 (XY)

Basic Characteristics

Diameter, mm 325

Length, mm 1,456

Weight, kg:

bomb 266

explosive 94 (XE)

PART 2  2

GROUP 13 AMMUNITION

AND EXPLOSIVES

Class 1325 Bombs

 13  !",  $" ! % 

! $&"$" $ ' $

 1325  

418

AIR BOMBS $%&%'(()* +',+)

GROUP 13 AMMUNITION

AND EXPLOSIVES

Class 1325 Bombs

 13  !",  $" ! % 

! $&"$" $ ' $

 1325  

()*+),- ./0/12-03(2313

-./,  400

-,  2425

,, 23:

 500

$$ 300 (67)

Basic Characteristics

Diameter, mm 400

Length, mm 2,425

Weight, kg:

bomb 500

explosive 300 (6E)

FAB-500M-62 HIGH EXPLOSIVE BOMB

This bomb is intended to engage military industrial

facilities, railway nodes, easily vulnerable and lightly

armored materiel, manpower, and field fortifications.

It is dropped from altitudes of 570 to 12,000 m at a

speed of 500 to 1,180 km/h.

DEF $!G!EEF H D-500 H-62

R/STU SV W/XV -W/Z[

\2., XTS/X[ ]T, 32]VT^  3-

2//^ .[2, X^ , -W[

/]X^. R/V.V  . 570 - 12000  W/ 2-

/.V[ 500 - 1180 2/U.

()*+),- ./0/12-03(2313

-./,  400

-,  2300

,, 23:

 515

$$ 230 (67)

Basic Characteristics

Diameter, mm 400

Length, mm 2,300

Weight, kg:

bomb 515

explosive 230 (6E)

OFAB-500U MULTIPURPOSE

HIGH EXPLOSIVE FRAGMENTATION BOMB

This bomb is intended to engage lightly armored and

easily vulnerable materiel, military industrial facilities,

railway nodes, field fortifications, and manpower. It

ensures above-surface instantaneous percussion, short

delay and delay action.

It is dropped from altitudes of 50 to 10,000 m at a

speed of 500 to 1,200 km/h.

E!$ IEF %IE-DEF

$!G!EEF H D-500

R/STU SV W/XV 32//^ 

32]VT^ .[2, -W/Z[ \2.,

XTS/X[ ]T, ^2[ _/._2[

/]X^, X^ . 'WU. SW/[.-

 3-2.2., TS, TS-

 S^..

R/V.V  . 50 - 10000  W/ 2/.V[ 500 -

1200 2/U.

PART 2  2

GROUP 13 AMMUNITION

AND EXPLOSIVES

Class 1325 Bombs

 13  !",  $" ! % 

! $&"$" $ ' $

 1325  

419

AIR BOMBS $%&%'(()* +',+)

()*+),- ./0/12-03(2313

-./,  500

-,  2280

,, 34:

 520

. 193

Basic Characteristics

Diameter, mm 500

Length, mm 2,280

Weight, kg:

bomb 520

filler 193

500-kg SIZE ODAB-500PM

FUEL-AIR EXPLOSIVE BOMB

This bomb is designed to engage manpower, industrial

facilities, vulnerable materiel and light engineer struc-

tures and to clear antipersonnel and antitank minefields.

It is dropped from altitudes of 200 to 1,000 m at a

speed of 500 to 1,100 km/h.

E FG-H G!I'J $!K!GGJ

F %L! 500 1M H-500F

L/MNO MP Q/RP RS , Q/T-

U /VRS, 43VPNS .U3, 43U R/-

U /VRS, /N/P Q/.QU.U 

Q/..3U U QS. L/P.P  . 200

- 1000  Q/ 3/.PU 500 - 1100 3/O.

500-kg SIZE BETAB-500ShP

CONCRETE-PIERCING BOMB

This bomb is designed to damage runways, taxiways,

highways and reinforced concrete shelters for aircraft.

It can demolish reinforced concrete runway surfaces of

up to 150 sq. m.

It is dropped from altitudes of 170 to 1,000 m at a

speed of 700 to 1,150 km/h.

 GNGJ $!K!GGJ F

%L! 500 1M  -500O

L/MNO MP Q/RP $LL [/M/, /VR-

U M/R3, ../M, RN.U V3/.S -

..

\N/VT. RN. Q3/.P $LL Q]M^_ M

150 

L/P.P  . 170 - 1000  Q/ 3/.PU 700 -

1150 3/O.

()*+),- ./0/12-03(2313

-./,  325

-,  2500

,, 34:

 380

$$ 107 (ab)

Basic Characteristics

Diameter, mm 325

Length, mm 2,500

Weight, kg:

bomb 380

explosive 107 (aE)

PART 2  2

GROUP 13 AMMUNITION

AND EXPLOSIVES

Class 1325 Bombs

 13  !",  $" ! % 

! $&"$" $ ' $

 1325  

420

AIR BOMBS $%&%'(()* +',+)

500-kg SIZE RBK-500 SPBE-D

CLUSTER BOMB LOADED

WITH HOMING ANTITANK

SENSOR-FUZED SUBMUNITIONS

WITH DUAL-MODE IR TARGET SEEKERS

This bomb is designed to defeat all modern tanks and other

armor materiel in the clutter and jamming environment.

It can simultaneously defeat up to six tanks. It is dropped

from altitudes of 400 to 5,000 m at a speed of 500 to

1,900 km/h.

&$4 5$4 %  %6! 500 78

$ 94: 9!! 5!; 6!$<'!5!4

!$9%$"5!  $"5! =6 5 95!,

9' 99"5! >$? :!59"5! !%

%>!95! ; 6! %-500 =->

CDEFG EH IDJH K DK LM

 EDNOP DDP LKM  NHK FEPLH

LLK  MNLK IK.

'ED JL IDJLQ E 6 LM. CDHLH

 L 400 - 5000  ID MDL 500 - 1900 M/G.

@ABCADE FGHG7IEHJ@IJ7J

TLD,  450

T,  2485

,, MO 500

GL K VL 15

Basic Characteristics

Diameter, mm 450

Length, mm 2,485

Weight, kg 500

Number of submunitions 15

PART 2  2

GROUP 13 AMMUNITION

AND EXPLOSIVES

Class 1325 Bombs

 13  !",  $" ! % 

! $&"$" $ ' $

 1325  

421

AIR BOMBS #$%$&''() *&+*(

500-kg SIZE RBK-500U

UNIFIED CLUSTER BOMB LOADED

WITH FRAGMENTATION, HIGH EXPLOSIVE

FRAGMENTATION, CONCRETE-PIERCING

AND ANTITANK SUBMUNITIONS

4!5!6!$447 &$7 8$7

%  %9! 500 :; (%-500)

$ 47> 4!! %94"8!, %94-

54"8!,  4?4"8!

! !$4%$"8!  $"8!

@9 8 48!