Каталог - Оружие России 2000 c82-795

Подождите немного. Документ загружается.

578

PART 4  4

LONG-RANGE AIR DEFENSE

MISSILE SYSTEMS

  

 !"# $ %!" 

ANTEY-2500 AIR DEFENSE MISSILE SYSTEM

Designed to defeat ground-based battlefield and theater

ballistic missiles with a launch range of up to 2,500 km,

aeroballistic and cruise missiles, strategic and tactical air-

craft, as well as loitering ECM platforms and high-precision

weapon systems in multiple air threat conditions, complex

air situation and severe ECM environment.

The Antey-2500 air defense missile system features:

- high degree of battle performance automation owing

to high-speed digital computers;

- phased-array radars;

- advanced radar data processing methods;

- high ECM immunity;

- high ability of autonomous operation;

- high mobility;

- high fire power potential, irrespective of air attack tac-

tics or sequence;

- vertical launch from a special transport launch

canister;

- maintenance-free operation of missiles for at least ten

years;

    «"-2500»

EFGHIJKIJLGIJ HMN OPFJQGIRN SJTSRLGUTRV R POGFJSRW-

IP-SJTSRLGUTRV XJMMRUSRLGUTRV FJTGS IJKGYIPZP XJKR-

FPWJIRN U HJM[IPUS[\ USJFSJ HP 2500 TY, J]FPXJMMR-

USRLGUTRV R TF^MJS^V FJTGS, UJYPMGSPW USFJSGZRLGUTP_

R SJTSRLGUTP_ JWRJ`RR, XJFFJQRFa\bRV OPUSJWbRTPW

OPYGV, W^UPTPSPLIPZP PFaQRN W aUMPWRNV YJUURFPWJI-

IPZP OFRYGIGIRN UFGHUSW WPKHacIPZP IJOJHGIRN, W

UMPQIP_ WPKHacIP_ R OPYGVPWP_ PXUSJIPWTG.

d  FGJMRKPWJI^:

- W^UPTJN USGOGI[ JWSPYJSRKJ`RR OFP`GUUPW XPGWP_ FJ-

XPS^ IJ PUIPWG X^USFPHG_USWa\bRV ed;

- OFRYGIGIRG fJKRFPWJII^V JISGII^V FGcGSPT IJ WUGV

FJHRPMPTJ`RPII^V UFGHUSWJV;

- UPWFGYGII^G UOPUPX^ PXFJXPSTR FJHRPMPTJ`RPII^V

URZIJMPW;

- W^UPTJN OPYGVPKJbRbGIIPUS[;

- W^UPTJN JWSPIPYIPUS[ W FJXPSG;

- W^UPTJN YPXRM[IPUS[;

- PZIGWJN OFPRKWPHRSGM[IPUS[ - IGKJWRURYJN PS SJTSRTR

HG_USWR_ d R OPUSFPGIRN IJMGSJ;

GROUP 14 GUIDED MISSILES

Class 1410 Guided Missile

Systems, Complete

()** 14 +  , 

 + (, *.+)

MJUU 1410 JTGSI^G R TPUYRLGUTRG URUSGY^ (TPYOMGTU^)

PYJIHI^_ OaITS

Command post

JHRPMPTJSPF TFaZPWPZP PXKPFJ

Circular scan radar

JHRPMPTJSPF UGTSPFIPZP PXKPFJ

Sector scan radar

, 0,,)1

AIR DEFENSE WEAPON SYSTEMS

579

PART 4  4

LONG-RANGE AIR DEFENSE

MISSILE SYSTEMS

  

 !"# $ %!" 

- WGFSRTJM[I^_ USJFS l RK UOG`RJM[IPZP SFJIUOPFSIP-

OaUTPWPZP TPISG_IGFJ;

- PSUaSUSWRG IGPXVPHRYPUSR SGVIRLGUTPZP PXUMaQRWJIRN

l W SGLGIRG IG YGIGG 10 MGS;

- WPKYPQIPUS[ OPFJQGIRN PSHGMN\bRVUN ZPMPWI^V LJU-

SG_ XJMMRUSRLGUTRV FJTGS U ]ffGTSRWIP_ OPWGFVIPUS[\

FJUUGNIRN XPMGG 0,02 Y

, MGSNbRV UP UTPFPUSNYR HP

4500 Y/UGT;

- PFRZRIJM[I^_ YGSPH IJWGHGIRN l - RIGF`RJM[I^_ U

FJHRPTPFFGT`RG_ R OPMaJTSRWI^Y UJYPIJWGHGIRGY IJ TP-

IGLIPY aLJUSTG OPMGSJ;

- IJOFJWMGII^_ OPHF^W XPGWP_ LJUSR l.

d UPUSJW URUSGY^ WVPHNS:

- TPYJIHI^_ OaITS;

- FJHRPMPTJSPF TFaZPWPZP PXKPFJ;

- FJHRPMPTJSPF UGTSPFIPZP PXKPFJ;

- YIPZPTJIJM[IJN USJI`RN IJWGHGIRN FJTGS () (4);

- OaUTPWJN aUSJIPWTJ 983 (El) (24);

- OaUTPKJFNQJ\bJN aUSJIPWTJ 984 (El) (24);

- KGIRSI^G aOFJWMNGY^G FJTGS^ 982;

- KGIRSI^G aOFJWMNGY^G FJTGS^ 983;

- YJcRI^ SGVIRLGUTPZP PXUMaQRWJIRN ( );

- YJcRI^ FGYPISJ R SGVIRLGUTPZP PXUMaQRWJIRN ( );

- ZFaOOPWP_ TPYOMGTS E;

- ]MGTSFPII^_ SFGIJQGF POGFJSPFPW ;

- SFJIUOPFSI^G YJcRI^;

- TPYOMGTS SJTGMJQIPZP PXPFaHPWJIRN U OJTGSJYR HMN

FJTGS.

- capability to defeat ballistic missile individual war-

heads featuring an effective reflective area (ERA) over

0.02 m

and flying at speeds of up to 4,500 m/s;

- inertial guidance with radio command update and

semiactive homing at the terminal phase;

- directional detonation of missile warhead.

The Antey-2500 system comprises:

- command post;

- circular scan radar;

- sector scan radar;

- multichannel missile guidance station (MMGS) (4);

- 9A83M launcher (24);

- 9A84M loader-launcher (24);

- 9M82M air defense missiles;

- 9M83M air defense missiles;

- maintenance vehicles;

- maintenance and repair vehicles;

- group SPTA set;

- electronic simulator for MMGS operator training;

- transporter vehicles;

- set of rigging equipment for handling missiles.

The 9M82M missile is intended to defeat battlefield,

the

ater and medium-range ballistic missiles, as well as

aerodynamic targets at a range of up to 200 km. The mis-

sile is controlled throughout the entire flight trajectory.

The 9M83M missile is intended to engage short- and

medium-range ballistic missiles and aerodynamic

targets.

GROUP 14 GUIDED MISSILES

Class 1410 Guided Missile

Systems, Complete

()** 14 +  , 

 + (, *.+)

MJUU 1410 JTGSI^G R TPUYRLGUTRG URUSGY^ (TPYOMGTU^)



MMGS

El

Loader-launchers

Launchers

580

PART 4  4

LONG-RANGE AIR DEFENSE

MISSILE SYSTEMS

  

 !"# $ %!" 

Antey-2500 system is mounted on tracked cross-coun-

try vehicles provided with self-contained power supply

systems and navigation, surveying and positioning

equipment.

A grouping, consisting

of several AD missile

systems, is controlled

by the Polyana-D4M1

AD brigade-level auto-

mated command post.

JTGS^ 982 OFGHIJKIJLGI^ HMN aIRLSPQGIRN SJTSRLG-

UTRV, POGFJSRWIP-SJTSRLGUTRV R UFGHIG_ HJM[IPUSR XJM-

MRUSRLGUTRV FJTGS, J SJTQG J]FPHRIJYRLGUTRV `GMG_ IJ

aHJMGIRR HP 200 TY. EFR ]SPY

FJTGSJ aOFJWMNGSUN IJ WUGY

aLJUSTG SFJGTSPFRR OPMGSJ.

JTGS^ 983 OFGHIJKIJLG-

I^ HMN aIRLSPQGIRN IJ YJM^V

R UFGHIRV HJM[IPUSNV SJTSRLG-

UTRV R POGFJSRWIP-SJTSRLG-

UTRV FJTGS, J SJTQG J]FPHRIJ-

YRLGUTRV `GMG_.

JKGYI^G XPGW^G UFGHUSWJ

FJKYGbJ\SUN IJ ZaUGIRLI^V

UJYPVPHI^V cJUUR W^UPTP_

OFPVPHRYPUSR, PUIJbGII^V

JWSPIPYI^YR URUSGYJYR

]MGTSFPUIJXQGIRN R JOOJFJ-

SaFP_ IJWRZJ`RR, SPOPOFRWNK-

TR R PFRGISRFPWJIRN.

lOFJWMGIRG XPGW^YR HG_USWR-

NYR ZFaOORFPWTR, UPUSPNbG_

RK IGUTPM[TRV , PUabGUSW-

MNGSUN JWSPYJSRKRFPWJIIP_

URUSGYP_ aOFJWMGIRN TPYJIH-

IPZP OaITSJ KGIRSIP_ FJTGSIP_

XFRZJH^ «EPMNIJ-%41».

GROUP 14 GUIDED MISSILES

Class 1410 Guided Missile

Systems, Complete

()** 14 +  , 

 + (, *.+)

MJUU 1410 JTGSI^G R TPUYRLGUTRG URUSGY^ (TPYOMGTU^)

,3456478 9:;:<=8;>3=><>

%JM[IPUS[ OPFJQJGY^V `GMG_, TY:

J]FPHRIJYRLGUTRV 200

XJMMRUSRLGUTRV HP 40

d^UPSJ OPFJQJGY^V `GMG_, TY:

J]FPHRIJYRLGUTRV 0,025 - 30

XJMMRUSRLGUTRV HP 30

JTURYJM[IJN UTPFPUS[ OPFJQGIRN , Y/U 4500

RIRYJM[IJN sE `GMG_, Y

0,02

JTURYJM[IJN HJM[IPUS[ USJFSJ OPFJQJGY^V , TY 2500

PMRLGUSWP PHIPWFGYGIIP PXUSFGMRWJGY^V `GMG_:

J]FPHRIJYRLGUTRV 24

XJMMRUSRLGUTRV 16

GYO USFGM[X^, U:

U FJKI^V OaUTPW^V aUSJIPWPT 0

U PHIP_ OaUTPWP_ aUSJIPWTR 1,5

dFGYN:

FJKWGFS^WJIRN/UWGFS^WJIRN XPGW^V UFGHUSW, YRI. 5/5

OPHZPSPWTR FJTGS^ T OaUTa, U 7,5

Basic Characteristics

Target engagement range, km:

aerodynamic targets 200

ballistic targets up to 40

Target engagement altitude, km:

aerodynamic targets 0.025 - 30

ballistic targets up to 30

Maximum target speed, m/s 4,500

Minimum target ERA, m

0.02

Maximum range to engage ballistic missiles, km 2,500

Number of simultaneously engaged targets:

aerodynamic 24

ballistic 16

Rate of fire, s:

several launchers 0

single launcher 1.5

Time into/out of action, min 5/5

Time to prepare missile for launch, s 7.5

581

PART 4  4

LONG-RANGE AIR DEFENSE

MISSILE SYSTEMS

  

 !"# $ %!" 

GROUP 14 GUIDED MISSILES

Class 1410 Guided Missile

Systems, Complete

 14    

  ( ")

6788 1410 79:;<=: > 9?8@>A:89>: 8>8;:@= (9?@C6:98=)

S-300P FAMILY AIR DEFENSE MISSILE SYSTEMS

Intended to defeat current and future aerial targets

under intensive ECM and multiple-threat environment,

such as:

- strategic, tactical and multirole aircraft; high-precision

weapon carrier aircraft, ECM platforms, AWACS air-

craft, as well as reconnaissance and strike aircraft,

including stealth aircraft;

- strategic cruise missiles, including those flying in

ter

rain-following mode at extremely low altitudes;

- ballistic-trajectory air-launched missiles;

- battlefield and theater ballistic missiles;

- antiradar missiles.

The S-300P AD missile system family incorporates the

S-300PMU, S-300PMU1 and S-300PMU2 air defense

missile systems.

Each system comprises:

- illumination and guidance radar (IGR);

- up to 12 transporter-launchers (TL);

- air defense missiles (ADM);

- technical support facilities;

- survey vehicle;

- set of service papers;

- individual SPTA set;

- power distribution/conversion devices furnished with

power cables.

Each system can operate as part of an air defense

grouping or independently with an attached target

acquisition radar. The standard air defense grouping

 *+ ,- -  -300

[\:]<7^<7A:<? ]6_ C?\7`:<>_ a b86?a>_c ><;:<8>a<?d?

\7]>?C\?;>a?]:e8;a>_ @788>\?a7<<=c b]7\?a 8?a\:@:<-

<=c > C:\8C:9;>a<=c 8\:]8;a a?^]bf<?d? <7C7]:<>_ a?

a8:c g?\@7c >c h?:a?d? C\>@:<:<>_:

- 87@?6:;?a 8;\7;:d>A:89?e > ;79;>A:89?e 7a>7i>>, @<?-

d?i:6:a?d? <7^<7A:<>_, <?8>;:6:e a=8?9?;?A<?d? ?\b-

`>_, C?8;7<?aj>9?a C?@:c, \7]>?6?97i>?<<?d? ]?^?\7 >

<7a:]:<>_, \7^a:]=a7;:6k<?-b]7\<=c 9?@C6:98?a, a ;?@

A>86: 87@?6:;?a, a=C?6<:<<=c C? ;:c<?6?d>> «8;:68»;

- 8;\7;:d>A:89>c 9\=67;=c \79:;, a ;?@ A>86: 8?a:\f7n-

j>c C?6:; <7 C\:]:6k<? @76=c a=8?;7c 8 ?d>h7<>:@

\:6k:g7 @:8;<?8;>;

- 7a>7i>?<<=c \79:; 8 h766>8;>A:89?e ;\7:9;?\>:e C?-

6:;7;

- ;79;>A:89>c > ?C:\7;>a<?-;79;>A:89>c h766>8;>A:89>c

\79:;;

- C\?;>a?\7]>?6?97i>?<<=c \79:;.

:@:e8;a?  -300[ a96nA7:; 8>8;:@= -300[o,

-300[o1 > -300[o2.

p 8?8;7a 97`]?e 8>8;:@= ac?]_;:

- \7]>?6?97;?\ C?]8a:;7 i:6:e > <7a:]:<>_ \79:; ([);

- ]? 12 ;\7<8C?\;<?-Cb89?a=c b8;7<?a?9 ([o);

- ^:<>;<=: bC\7a6_:@=: \79:;= (o);

- 8\:]8;a7 ;:c<>A:89?d? ?h:8C:A:<>_ q98C6b7;7i>>

\79:;;

- ;?C?C\>a_^A>9;

- 9?@C6:9; q98C6b7;7i>?<<?e ]?9b@:<;7i>>;

- [ ?]><?A<=e;

[

IGR

GROUP 14 GUIDED MISSILES

Class 1410 Guided Missile

Systems, Complete

 14    

  ( ")

6788 1410 79:;<=: > 9?8@>A:89>: 8>8;:@= (9?@C6:98=)

582

PART 4  4

LONG-RANGE AIR DEFENSE

MISSILE SYSTEMS

  

 !"# $ %!" 

comprises command/control assets (CCA) and up to

six AD missile systems. The following grouping version-

s may be fielded:

- 83M6E command/control assets and up to six

S-300PMU1, S-300PMU and S-200VE AD missile

systems;

- 83M6E2 command/control assets and up to six

S-300PMU2, S-300PMU1, S-300PMU and S-200VE

(Favorit) AD missile systems.

The air defense groupings, comprising 83M6E com-

mand/control assets and up to six S-300PMU1,

S-300PMU and Favorit AD missile systems (83M6E2

command/control assets and up to six S-300PMU2,

S-300PMU1 and S-300PMU AD missile systems), can

simultaneously engage up to 36 targets by 72 missiles.

The command/control assets comprise:

- combat control post (CCP);

- target acquisition radar (TAR);

- survey vehicle;

- set of service papers;

- \78C\:]:6>;:6k<?-C\:?h\7^?a7;:6k<=: b8;\?e8;a7

([o) 8 9?@C6:9;7@> 8>6?a=c 97h:6:e.

7`]7_  @?`:; gb<9i>?<>\?a7;k 979 a 8?8;7a: d\bC-

C>\?a9> [p , ;79 > 7a;?<?@<? 8 C\>]7a7:@?e !

?h<7\b`:<>_. p 8?8;7a ;>C?a?e d\bCC>\?a9> ac?]_; 8\:]-

8;a7 bC\7a6:<>_ (o) > ]? f:8;> . p?^@?`<=: a7\>-

7<;= 8?8;7a7 d\bCC>\?a?9:

- o 836 > ]? f:8;>  -300[o1, -300[o,

-200pu;

- o 8362 > ]? f:8;>  -300[o2, -300[o1,

-300[o, -200pu (8>8;:@7 [p «v7a?\>;»);

w\bCC>\?a9> [p , a96nA7nj>: o 836, ]? f:8;> 

-300[o1, -300[o > 8>8;:@b [p «v7a?\>;»

(o 8362 > ]? f:8;>  -300[o2, -300[o1,

-300[o), ?h:8C:A>a7n; ?h8;\:6 ]? 36 i:6:e, ?]<?a\:-

@:<<? <7c?]_j>c8_ a a?^]bc:, 8 <7a:]:<>:@ <7 <>c ]?

72 \79:;.

p 8?8;7a 8\:]8;a bC\7a6:<>_ ac?]_;:

- Cb<9; h?:a?d? bC\7a6:<>_ ([o);

- \7]>?6?97;?\ ?h<7\b`:<>_ (! );

[o

o

ADM

583

PART 4  4

LONG-RANGE AIR DEFENSE

MISSILE SYSTEMS

  

 !"# $ %!" 

GROUP 14 GUIDED MISSILES

Class 1410 Guided Missile

Systems, Complete

 14    

  ( ")

6788 1410 79:;<=: > 9?8@>A:89>: 8>8;:@= (9?@C6:98=)

- ;?C?C\>a_^A>9;

- 9?@C6:9; q98C6b7;7i>-

?<<?e ]?9b@:<;7i>>;

- [ ?]><?A<=e > d\bC-

C?a?e;

- \78C\:]:6>;:6k<?-C\:-

?h\7^?a7;:6k<=: b8;\?e-

8;a7 8 9?@C6:9;7@> 8>-

6?a=c 97h:6:e.

h@:< ><g?\@7i>:e

@:`]b <7^:@<=@> h?:-

a=@> 8\:]8;a7@> d\bC-

C>\?a9> ?8bj:8;a6_:;8_

C? ;:6:9?]?a=@ 6><>_@

8a_^>, \7h?;7nj>@ a

\:`>@7c «\7]>?» >6>

«C\?a?]».

o >  @?db; h=;k

\7^<:8:<= <7 \788;?_-

<>: ]? 50 9@ C\> >8C?6k-

^?a7<>> \:;\7<86_;?\?a

>6> \7]>?\:6:e<=c

8;7<i>e > ]? 100 9@ -

C\> >8C?6k^?a7<>> C\?-

a?]<?e 8a_^>.

u6:9;\?8<7h`:<>: o

>  - ?; a8;\?:<<=c

7a;?<?@<=c 8\:]8;a, a=-

C?6<:<<=c <7 ?8<?a: d7-

^?;b\h><<=c 7d\:d7;?a,

7 ;79`: ?; C\?@=f6:<-

<?e 8:;> > C\>]7a7:@=c

]>^:6k-q6:9;\?8;7<i>e

A:\:^ \78C\:]:6>;:6k-

<?-C\:?h\7^?a7;:6k<=:

b8;\?e8;a7.

8<?a<?e ;\7<8C?\;<?e

:]><>i:e o >  _a-

6_:;8_ 7a;?@?h>6k<?:

f788> a=8?9?e C\?c?]>-

@?8;> -543. [\:-

]b8@?;\:<? \7^@:j:<>:

o >  <7 8;7i>?<7\-

<=c C?^>i>_c.

o >  - a8:C?d?]<=,

q98C6b7;>\bn;8_ a \7^-

6>A<=c 96>@7;>A:89>c

^?<7c.

- group and individual

SPTA sets;

- power distribution/con-

version devices

furnished with power

cables.

The data exchange

between grouping com-

bat assets is carried out

via coded telemetry

channels in the «radio»

or «wire» operating

mode.

The command/control

assets and air defense

missile systems can be

separated to a distance

of up to 50 km when

using repeater and radio

relay stations and up to

100 km when using wire

communications.

The command/control

assets and air defense

missile systems are

supplied with electric

power from self-con-

tained power supply

sources built around

gas-turbine generating

units, as well as from

industrial power supply

mains and diesel power

plants via distribu-

tion/conversion devices.

The command/control

assets and air defense

missile systems are

mounted on the

MAZ-543M cross-

country motor-vehicle

chassis. Provision is

made for their station-

ary basing.

The command/control

assets and air defense

missile systems are of

the all-weather type and

can be operated in var-

ious climates.

!

TAR

[o

CCP

584

PART 4  4

LONG-RANGE AIR DEFENSE

MISSILE SYSTEMS

  

 !"# $ %!" 

GROUP 14 GUIDED MISSILES

Class 1410 Guided Missile

Systems, Complete

 14    

  ( ")

6788 1410 79:;<=: > 9?8@>A:89>: 8>8;:@= (9?@C6:98=)

Combat assets complement

ADM systems

S-300PMU S-300PMU1 S-300PMU2

IGR 30N6 30N6E, 30N6E1 30N6E2

TL 5P85SU, 5P85DU 5P85SE, 5P85TU 5P85SE2, 5P85TE2

ADM 5V55R, 5V55K 48N6E 48N6E2, 48N6E

Basic Characteristics

S-300PMU S-300PMU1 S-300PMU2

Number of:

simultaneously

engaged targets up to 6 up to 6 up to 6

simultaneously

guided missiles up to 12 up to 12 up to 12

Target engagement envelope, km:

aerodynamic targets:

range 5 - 90 5 - 150 3 - 200

(by 5V55R ADM), (head-on (head-on

5 - 50 (by 5V55K ADM) and pursuit) and pursuit)

altitude 0.025 - 25 0.01 - 27 0.01 - 27

cross-range - 149 195

ballistic targets:

range 5 - 35 5 - 40 5 - 40

altitude - 2 - 25 2 - 25

cross-range - - 25 - 35

Target speed, m/s 50-1,200 0-2,800 0-2,800

Measurement accuracy:

range, m 5 5 5

speed, m/s 1 1 1

angular coordinate difference,

arcmin 1 1 1

Sectors of autonomous detection

(elevation x azimuth), deg:

low-flying targets 1 x 105 1 x 90 1 x 90

medium- and high-altitude

aerodynamic targets 4 x 12 5 x 64, 14 x 64 5 x 64, 14 x 64

ballistic targets - 10 x 32 10 x 32

Time of:

response to target data

from CCA, s 9 - 11 9 - 11 9 - 11

deployment

(closing-down), min 5 5 5

Rate of fire, s 3 - 5 3 - 5 3 - 5

Vehicle movement speed, km/h:

on highway 60 60 60

on dirt road 30 30 30

Fuel distance, km 800 800 800

Service life, years 20 20 20

Combat crew 6 6 6

?@ABC D?ECFG @HEI@AC

 -300[o -300[o1 -300[o2

[ 306 306, 3061  62

[o 5[85o, 5[85%o 5[85, 5[85 5[852, 5[852

o 5p55, 5p55 486 4862, 486

@J?CJFE GBHBKAEHL@ALKL

 -300  -300 1 -300 2

?6>A:8;a?:

C?\7`7:@=c i:6:e,

?]<?a\:@:<<?

<7c?]_j>c8_ a C?6:;: ]? 6 ]? 6 ]? 6

?]<?a\:@:<<?

<7a?]>@=c \79:; ]? 12 ]? 12 ]? 12

?<7 C?\7`:<>_, 9@:

7q\?]><7@>A:89>c i:6:e:

C? ]76k<?8;> 5-90 - 5-150 3-200

\79:;?e 5p55, (<7 a8;\:A<=c (<7 a8;\:A<=c

5-50 - \79:;?e 9b\87c > a]?d?<) 9b\87c > a]?d?<)

5p55

C? a=8?;: 0,025-25 0,01-27 0,01-27

9b\8?a?e C7\7@:;\ - 149 195

h766>8;>A:89>c i:6:e:

C? ]76k<?8;> 5-35 5-40 5-40

C? a=8?;: - 2-25 2-25

9b\8?a?e C7\7@:;\ - - 25 - 35

9?\?8;> C?\7`7:@=c

i:6:e, @/8 50-1200 0-2800 0-2800

?A<?8;> >^@:\:<>_:

]76k<?8;k, @ 5 5 5

89?\?8;k, @/8 1 1 1

\7^<?8;> bd6?a=c

9??\]><7;, @><. 1 1 1

:9;?\7 7a;?<?@<?d?

?h<7\b`:<>_ (bd?6 @:8;7 c 7^>@b;), d\7].:

C? <>^9?6:;_j>@

i:6_@ 1 c 105 1 c 90 1 c 90

C? 7q\?]><7@>A:89>@

i:6_@ <7 8\:]<>c

> h?6kf>c a=8?;7c 4 c 12 5 c 64, 14 c 64 5 c 64, 14 c 64

C? h766>8;>A:89>@ i:6_@ - 10 c 32 10 c 32

p\:@_:

\:79i>> C\>

i:6:b97^7<>> ?; o, 8 9 - 11 9 - 11 9 - 11

\7^a:\;=a7<>_

(8a:\;=a7<>_), @><. 5 5 5

:@C 8;\:6kh=, 8 3 - 5 3 - 5 3 - 5

9?\?8;k C:\:]a>`:<>_

h?:a=c 8\:]8;a, 9@/A:

C? f?88: 60 60 60

C? d\b<;?a=@ ]?\?d7@ 30 30 30

7C78 c?]7 h:^

]?^7C\7a9> 8\:]8;a, 9@ 800 800 800

u98C6b7;7i>?<<=e

8\?9 86b`h=, d?]= 20 20 20

?:a?e \78A:;, A:6. 6 6 6

585

PART 4  4

LONG-RANGE AIR DEFENSE

MISSILE SYSTEMS

  

 !"# $ %!" 

GROUP 14 GUIDED MISSILES

Class 1410 Guided Missile

Systems, Complete

 14    

  ( ")

6788 1410 79:;<=: > 9?8@>A:89>: 8>8;:@= (9?@C6:98=)

?@ABC D?ECFG @HEI@AC

o 836 8362

[o 546 5462

! 646 6462

@J?CJFE GBHBKAEHL@ALKL

o 83 6 83 62

?6>A:8;a? ?]<?a\:@:<<?:

bC\7a6_:@=c  6 6

?h<7\b`>a7:@=c i:6:e 300 300

8?C\?a?`]7:@=c ;\788 100 100

i:6:b97^7<>e 36 36

<8;\b@:<;76k<7_ ]76k<?8;k ! , 9@ 300 300

?<= \:db6_\<?d? ?h^?\7 ! , d\7].:

C? 7^>@b;b

0 - 360 >6> 0 - 180 0 - 360 >6> 0 - 180

C? bd6b @:8;7

0 - 14 >6> 0 - 28 0 - 14 >6> 0 - 28

:9;?\ ?h<7\b`:<>_

h766>8;>A:89>c i:6:e, d\7].:

C? 7^>@b;b ]? 60 60

C? bd6b @:8;7 0 - 55 >6> 20 - 75 0 - 75

9?\?8;k:

?h<7\b`>a7:@=c i:6:e, @/8 ]? 2800 ]? 2800

C:\:]a>`:<>_, 9@/A:

C? f?88: 60 60

C? d\b<;?a=@ ]?\?d7@ 30 30

?A<?8;k >^@:\:<>_:

7^>@b;7, d\7]. 0,5 0,5

bd67 @:8;7, d\7]. 0,5 0,5

]76k<?8;>, @ 150 150

p\:@_ \7^a:\;=a7<>_ (8a:\;=a7<>_), @><. 5 5

7C78 c?]7 h:^ ]?^7C\7a9>, 9@ 800 800

u98C6b7;7i>?<<=e 8\?9 86b`h=, d?]= 20 20

?:a?e \78A:;, A:6. 5 5

Command/control assets complement

CCA 83M6E 83M6E2

CCP 54K6E 54K6E2

TAR 64N6E 64N6E2

Basic Characteristics

CCA 83M6E 83M6E2

Number of simultaneously:

controlled AD missile systems 6 6

detected targets 300 300

tracked targets 100 100

designated targets 36 36

Target acquisition range, km 300 300

Scanned area, deg:

azimuth

0 - 360 or 0 - 180 0 - 360 or 0 - 180

elevation

0 - 14 or 0 - 28 0 - 14 or 0 - 28

Ballistic target detection sector, deg:

azimuth up to 60 60

elevation 0 - 55 or 20 - 75 0 - 75

Speed of:

detected targets, m/s up to 2,800 up to 2,800

vehicle movement, km/h:

on highway 60 60

on dirt road 30 30

Measurement accuracy:

azimuth, deg 0.5 0.5

elevation, deg 0.5 0.5

range, m 150 150

Time of deployment (closing-down), min 5 5

Fuel distance, km 800 800

Service life, years 20 20

Combat crew 5 5

586

PART 4  4

LONG-RANGE AIR DEFENSE

MISSILE SYSTEMS

  

 !"# $ %!" 

TRIUMPH AIR DEFENSE SYSTEM

Intended to repulse

mass attacks delivered

by current and future

air attack weapons.

The Triumph system

incorporates com-

mand/control assets

and air defense medi-

um- and long-range

missile systems (up to

eight ADM systems)

developed from the

most recent research

and engineering

achievements in elec-

tronics, computer

engineering, rocketry,

with the use of

advanced circuitry and

technologies, as well

as the most sophisti-

cated software for the

ground-based and

onboard computer

systems.

The Triumph system’s

architecture is similar

to that of the Favorit

air defense system,

but significantly out-

performs it in terms of

the following basic

performance charac-

teristics:

- maximum target engaging ranges and altitudes;

- target/missile channel capacity;

- jamming immunity of ground-based and onboard

electronic facilities;

- high fire power potential;

- maximum target speed (5,000 m/s) that correspond-

s to nonstrategic ballistic missiles with a range of up to

3,500 km.

The system is provided with improved transportation

facilities: chassis equipped with a power generating

unit driven by the cruise engine.

The Triumph system may be used to form air defense

groupings incorporating the S-300P and other AD mis-

sile systems.

The Triumph system command/control assets and AD

missiles can cooperate with various automated control

systems and radar facilities.

Along with the new AD missiles the system can use the

S-300PMU AD missiles. The possibility of using AD mis-

siles with various effective ranges ensures the system

modular capability that makes it possible to set up lay-

ered air defense and nonstrategic antimissile defense

systems. The mixed ammunition load allows for opti-

mum use of ammunition (in terms of effectiveness-cost

ratio).

  «»

KLMNOPQOPRMOP NST UV-

LPWMOXT YPZZXLU[POO\]

^NPLU[ [ZM] ZU[LMYMO-

O\] X _MLZ_M`VX[O\]

ZLMNZV[ [UQN^aOUbU OP-

_PNMOXT.

c ZUZVP[ ZXZVMY\ «LX-

^Ye» []UNTV ZLMNZV[P

^_LP[SMOXT (g) X QM-

OXVO\M LP`MVO\M ZXZ-

VMY\ () hUSiaUj X

ZLMNOMj NPSiOUZVX,

LPQLPhUVPOO\M OP UZOU-

[M OU[MjaX] OP^ROU-

VM]OXRMZ`X] NUZVXWM-

OXj [ LPNXUVM]OX`M, [\-

RXZSXVMSiOUj VM]OX`M,

LP`MVUZVLUMOXX, Z _LX-

YMOMOXMY _MLZ_M`VX[-

OUj kSMYMOVOUj hPQ\ X

_LUbLMZZX[O\] VM]OUSU-

bXj, Z `PRMZV[MOOU OU-

[\Y _LUbLPYYOU-PSbU-

LXVYXRMZ`XY UhMZ_MRM-

OXMY OPQMYO\] X hULVU-

[\] [\RXZSXVMSiO\]

`UY_SM`ZU[.

XZVMYP «LX^Ye» XYM-

MV PL]XVM`V^L^ _UZVLUM-

OXT, _UNUhO^l ZXZVMYM

Kc «mP[ULXV», Z^nM-

ZV[MOOU _LM[UZ]UNT MM

_U ZSMN^lnXY UZOU[-

O\Y VP`VX`U-VM]OXRMZ`XY ]PLP`VMLXZVX`PY:

- YP`ZXYPSiO\M NPSiOUZVi X [\ZUVP _ULPWPMY\] oMSMj;

- `POPSiOUZVi _U oMSTY X LP`MVPY;

- _UYM]UQPnXnMOOUZVi OPQMYO\] X hULVU[\] LPNXUkSM`-

VLUOO\] ZLMNZV[;

- UbOM[PT _LUXQ[UNXVMSiOUZVi;

- YP`ZXYPSiOPT Z`ULUZVi _ULPWPMY\] oMSMj - 5000 Y/Z,

RVU ZUUV[MVZV[^MV OMZVLPVMbXRMZ`XY hPSSXZVXRMZ`XY LP-

`MVPY Z NPSiOUZVil _^Z`P NU 3500 `Y.

c ZXZVMY^ [[UNXVZT ^ZU[MLaMOZV[U[POOPT VLPOZ_ULVOPT

hPQP Z kOMLbUZOPhWMOXMY QP ZRMV UVhULP YUnOUZVX UV

YPLaM[UbU N[XbPVMST aPZZX.

P MM UZOU[M YUb^V eULYXLU[PViZT bL^__XLU[`X Kc Z

XZ_USiQU[POXMY, [ VUY RXZSM, 3PC ZMYMjZV[P -300K X

NL^bX] .

g X  ZXZVMY\ «LX^Ye» Z_UZUhO\ [QPXYUNMjZV-

[U[PVi Z LPQSXRO\YX P[VUYPVXQXLU[POO\YX ZXZVMYP-

YX ^_LP[SMOXT X ZLMNZV[PYX LPNXUSU`PoXUOOUbU _U-

ST.

c ZXZVMYM OPLTN^ Z OU[\YX LP`MVPYX _LXYMOTlVZT LP-

`MV\  ZMYMjZV[P -300Kg. cUQYUWOUZVi XZ_USiQU-

[POXT LP`MV Z LPQSXROUj NPSiOUZVil NMjZV[XT UhMZ_M-

RX[PMV YUN^SiOUZVi, RVU _UQ[USTMV UZ^nMZV[STVi kaM-

SUOXLU[POOUM _UZVLUMOXM _LUVX[U[UQN^aOUj X OMZVLP-

VMbXRMZ`Uj _LUVX[ULP`MVOUj UhULUO\. KLX ZYMaPOOUY

eULYXLU[POXX hUM`UY_SM`VP NUZVXbPMVZT MbU U_VXYPSi-

OUM LPZ]UNU[POXM _U `LXVMLXl «keeM`VX[OUZVi - ZVUX-

YUZVi».

GROUP 14 GUIDED MISSILES

Class 1410 Guided Missile

Systems, Complete

% 14 &'(  &&

( (&*&()

SPZZ 1410 P`MVO\M X `UZYXRMZ`XM ZXZVMY\ (`UY_SM`Z\)

587

PART 4  4

LONG-RANGE AIR DEFENSE

MISSILE SYSTEMS

  

 !"# $ %!" 

MODERNIZATION OF S-200VE

AIR DEFENSE MISSILE SYSTEM

The modernization involves:

- introduction of the 5V28M missile into the system

complement to increase its target engagement range;

- formation of ADM batteries deployed at a distance of

up to 100 km from targeting systems;

- equipping the target illumination and guidance radar

with a sound indication channel to discriminate target

classes;

- introduction of linear frequency-modulated signal

illumination and reception modes to engage targets

with low radial rates.

The offered modernization package can be specified

at customer request.

 !"#!$

" -200%&

EFGEHIJKLM NOPJGKLQERLL:

- HHOP H  GESJTU 5V28 PIM GEWXLGJKLM QOKU FOGE-

YJKLM RJIJZ FO PEI[KOWTL;

- WOQPEKLJ HUKJWJKKU\ QJKLTKU\ GESJTKU\ ]ETEGJZ, _PE-

IJKKU\ OT LK`OGNERLOKKU\ WGJPWTH KE GEWWTOMKLM PO

100 SN;

- HHJPJKLJ H GEPLOIOSETOG FOPWHJTE RJIL EFFEGET_GU

QH_SOHOZ LKPLSERLL PIM GEWFOQKEHEKLM SIEWWOH RJIJZ;

- GJEILQERLM GJYLNOH LQI_aJKLM L FGLJNE WLbKEIOH W

ILKJZKOZ aEWTOTKOZ NOP_IMRLJZ PIM O]WTGJIE RJIJZ W

NEIUNL GEPLEI[KUNL WSOGOWTMNL.

cGJPIEbEJNUJ KEFGEHIJKLM NOb_T _TOaKMT[WM L POFOI-

KMT[WM FO WObIEWOHEKLd W QESEQaLSON.

GROUP 14 GUIDED MISSILES

Class 1410 Guided Missile

Systems, Complete

*+,, 14 - . ! -!-!

!. (-,0-.)

IEWW 1410 ESJTKUJ L SOWNLaJWSLJ WLWTJNU (SONFIJSWU)