Каталог - Оружие России 2000 c82-795

  1. Файлы
  2. Академическая и специальная литература
  3. Военные дисциплины
  4. Оружие и военная техника
  5. Энциклопедии, словари, справочники
Назад
588
PART 4  4
MEDIUM-RANGE AIR DEFENSE
MISSILE SYSTEMS
   
!" !# 
GROUP 14 GUIDED MISSILES
Class 1410 Guided Missile
Systems, Complete
 14   
  ( ")
5677 1410 689:;<9 = 8>7?=@978=9 7=7:9?< (8>?B5987<)
$% %  " «'- 1-2»
D9E;6F;6@9; E5G B>D6H9;=G 76?>59:>I :68:=@978>J =
7:D6:9K=@978>J 6I=6L==, 8D<56:<M D689:, I9D:>59:>I =
EDNK=M 6OD>E=;6?=@978=M >PQ98:>I I> I79? E=6B6F>;9 =M
BD68:=@978>K> BD=?9;9;=G I N75>I=GM =;:9;7=I;>K> D6-
E=>BD>:=I>E9J7:I=G, 6 :68H9 E5G P>DRP< 7 :68:=@978=?=
P655=7:=@978=?= D689:6?= :=B6 «6;7», BD>:=I>D6E=>5>-
86L=>;;<?= D689:6?= :=B6 «U6D?» = EDNK=?= O59?9;:6?=
I<7>8>:>@;>K> >DNH=G I>FENV;>K> = ;6F9?;>K> P6F=D>-
I6;=G, B>D6H9;=G ;6EI>E;<M = >P7:D956 ;6F9?;<M D6E=>-
8>;:D67:;<M L959J.
 >P97B9@=I69::
- ;6E9H;NY BD>:=I>I>FENV;NY >P>D>;N I>J78 I D6F5=@-
;<M N75>I=GM = I=E6M P>9I<M E9J7:I=J, 6 :68H9 I6H;<M
6E?=;=7:D6:=I;>-BD>?<V59;;<M >PQ98:>I 7 >E;>ID9-
?9;;<? >P7:D95>? E> 6 L959J 7 5YP<M ;6BD6I59;=J;
- I<7>8NY B>?9M>N7:>J@=I>7:R I N75>I=GM =;:9;7=I;>K>
D6E=>BD>:=I>E9J7:I=G;
- I<7>8=9 I>F?>H;>7:= =;:9KD6L== I D6F5=@;<M KDNBB=-
D>I8= \;
- O]]98:=I;NY F6^=:N >: I<7>8>:>@;>K> >DNH=G;
- I79B>K>E;>7:R, I<7>8NY ?>P=5R;>7:R, BD>M>E=?>7:R,
?65>9 ID9?G D6FI9D:<I6;=G = 7I9D:<I6;=G;
- O87B5N6:6L=Y I D6F5=@;<M 85=?6:=@978=M N75>I=GM;
- I>F?>H;>7:R 6I:>;>?;>K> I9E9;=G P>9I<M E9J7:I=J;
- O87B5N6:6L=Y D689: P9F :9M;=@978>K> >P75NH=I6;=G I
:9@9;=9 10 59:.
\ 7>7:6I  IM>EG::
- 8>?6;E;<J BN;8: () 9 4701-2;
- 7:6;L=G >P;6DNH9;=G L959J ( b) 9 181-1;
- 76?>M>E;6G >K;9I6G N7:6;>I86 ( c) 93101-2 (E>
6 V:N8) 7 4 D689:6?=;
- BN78>-F6DGH6Y^6G N7:6;>I86 (c) 9391 (E> 6 V:N8)
7 8 D689:6?=;
- F9;=:;<9 NBD6I5G9?<9 D689:< (c) 9317 =5=
9381;
BUK-M1-2 AIR DEFENSE MISSILE SYSTEM
Intended to defeat tactical and strategic aircraft, cruise mis-
siles, helicopters and other aerodynamic targets throughout
the entire range of their combat employment in severe ECM
environment, as well as Lance-type tactical ballistic missiles,
HARM-type antiradar missiles and other airborne and ground-
based high-precision weapons and engage water-borne and
radio-contrast ground targets.
The system provides:
- reliable air defense of troops in all kinds of combat action,
as well as vital administrative and industrial facilities, simulta-
neously engaging up to six targets flying from any direction;
- high jamming immunity in severe ECM environment;
- high capability of integrating with any air defense grouping;
- effective protection against high-precision weapons;
- all-weather capability, high mobility and cross-country per-
formance, short deployment (closing-down) time;
- capability of operation in any climatic conditions;
- autonomous combat capability;
- maintenance-free operation of the missiles for ten years.
The system comprises:
- 9S470M1-2 command post (CP);
- 9S18M1-1 target acquisition radar (TAR);
- up to six 9A310M1-2 self-propelled mounts (SPM) with four
missiles;
 9 4701-2
9S470M1-2 CP
b 1 181-1
1S18M1-1 TAR
589
PART 4  4
MEDIUM-RANGE AIR DEFENSE
MISSILE SYSTEMS
   
!" !# 
GROUP 14 GUIDED MISSILES
Class 1410 Guided Missile
Systems, Complete
 14   
  ( ")
5677 1410 689:;<9 = 8>7?=@978=9 7=7:9?< (8>?B5987<)
c 93101-2 7 c 9317
9A310M1-2 SPM with 9M317 ADMs
c 9391 7 c 9381
9A39M1 launcher-loader with 9M38M1 ADMs
- ?6V=;6 :9M;=@978>K> >P75NH=I6;=G () 9\881 7 BD=-
L9B>?  9456;
- ?67:9D786G :9M;=@978>K> >P75NH=I6;=G -t-1;
- ?6V=;< D9?>;:6 = :9M;=@978>K> >P75NH=I6;=G (-1)
9\8831, (-2) 9\8841, (-3) 9\8941;
- up to six 9A39M1 launcher-loaders (LL) with eight missiles;
- 9M317 or 9M38M1 AD missiles;
- 9V881 maintenance vehicle with 9T456 SPTA trailer;
- MTO-ATG-M1 maintenance workshop;
- 9V883M1 (MRTO-1), 9V884M1 (MRTO-2) and 9V894M1
590
PART 4  4
MEDIUM-RANGE AIR DEFENSE
MISSILE SYSTEMS
   
!" !# 
Basic Characteristics
9M38M1 ADM 9M317 ADM
Target engagement envelope, km:
aerodynamic targets (ERA = 1 m
2
):
range 3 - 32 3 - 42
altitude 0.015 - 22 0.015 - 25
maximum cross-range 22 25
Lance-2 type tactical ballistic missiles:
far boundary - 20
maximum altitude - 16
maximum cross-range - 14
ALCM-type cruise missile engagement
range at altitudes, km:
30 m 3 - 9.5 3 - 12
6 km 3 - 26 3 - 28
maximum cross-range 10 15
Range, km:
firing at surface targets:
destroyer - 3 - 25
missile boat - 3 - 18
ground-based radio-contrast targets - 3 - 15
Number of simultaneously engaged targets 6 6
Single-shot kill probability:
aerodynamic targets 0.7 - 0.9 0.7 - 0.9
Lance-2 type tactical ballistic missiles - 0.5 - 0.7
HARM type antiradar missiles - 0.6 - 0.8
cruise missiles, including ALCM not less than 0.4 0.7 - 0.8
flying helicopters 0.3 - 0.7 0.7 - 0.8
hovering helicopters 0.3 - 0.4 0.3 - 0.4
Maximum target speed, m/s 830 1,200
Maximum target g-load, g 10 12
Number of missiles:
9A310M1-2 self-propelled launcher 4 4
9A39M1 launcher-loader 8 8
Response time, s 15 - 18 15 - 18
Time of deployment from march, min 5 5
=>?@>AB CDEDFGBEH=GHFH
$ 9 38 1 $ 9 317
>;6 B>D6H9;=G, 8?:
6OD>E=;6?=@978=9 L95= (y=1 ?
2
)
B> E65R;>7:= 3 - 32 3 - 42
B> I<7>:9 0,015 - 22 0,015 - 25
?687=?65R;<J 8ND7>I>J B6D6?9:D 22 25
:68:=@978=9 P655=7:=@978=9 D689:< :=B6 «6;7-2»
E65R;GG KD6;=L6 - 20
?687=?65R;6G I<7>:6 - 16
?687=?65R;<J 8ND7>I>J B6D6?9:D - 14
!65R;>7:R 7:D95RP< B> 8D<56:<? D689:6?
:=B6  ;6 I<7>:6M, 8?:
30 ? 3 - 9,5 3 - 12
6 8? 3 - 26 3 - 28
BD= ?687=?65R;>? 8ND7>I>? B6D6?9:D9 10 15
!65R;>7:R, 8?:
7:D95RP< B> ;6EI>E;<? L95G?:
:=B6 O7?=;9L - 3 - 25
:=B6 D689:;<J 86:9D - 3 - 18
>P7:D956 ;6F9?;<M D6E=>8>;:D67:;<M L959J - 3 - 15
>5=@97:I> >E;>ID9?9;;> >P7:D95=I69?<M L959J
6 6
\9D>G:;>7:R B>D6H9;=G >E;>J D689:>J:
6OD>E=;6?=@978=M L959J 0,7 - 0,9 0,7 - 0,9
:68:=@978=M P655=7:=@978=M D689: :=B6 «6;7-2»
- 0,5 - 0,7
BD>:=I>D6E=>5>86L=>;;<M D689: :=B6 «U6D?»
- 0,6 - 0,8
8
D<56:<M D689:, I :>? @=759 :=B6 
;9 ;=H9 0,4 0,7 - 0,8
59:G^=M I9D:>59:>I 0,3 - 0,7 0,7 - 0,8
F6I=76Y^=M I9D:>59:>I 0,3 - 0,4 0,3 - 0,4
687=?65R;6G 78>D>7:R B>D6H69?<M L959J, ?/7
830 1200
687=?65R;6G B9D9KDNF86 B>D6H69?<M L959J, 9E.
10 12
>5=@97:I> D689::
;6 c 93101-2 4 4
;6 c 9391 8 8
\D9?G D968L==, 7 15 - 18 15 - 18
\D9?G D6FI9D:<I6;=G 7 ?6DV6, ?=;. 5 5
GROUP 14 GUIDED MISSILES
Class 1410 Guided Missile
Systems, Complete
 14   
  ( ")
5677 1410 689:;<9 = 8>7?=@978=9 7=7:9?< (8>?B5987<)
- :D6;7B>D:;<9 ?6V=;< () 9243 7 8>?B598:>? :9M;>-
5>K=@978>K> >P>DNE>I6;=G () 9318.
!5G NBD6I59;=G P>9I<?= E9J7:I=G?= KDNBB=D>I8=,
7>7:>G^9J =F ;978>5R8=M (E> @9:<D9M)  «zN8-1-2»
BD=?9;G9:7G 6I:>?6:=F=D>I6;;6G 7=7:9?6 NBD6I59;=G
8>?6;E;>K> BN;8:6 F9;=:;>J D689:;>J PD=K6E<
«>5G;6-!41».
(MRTO-3) repair and maintenance vehicles;
- 9T243 transport vehicles with a set of 9T318 maintenance
equipment.
The Polyana-D4M1 automated control system of the AD mis-
sile brigade command post is used to control combat action-
s of a grouping comprising up to four Buk-M1-2 air defense
missile systems.
591
PART 4  4
MEDIUM-RANGE AIR DEFENSE
MISSILE SYSTEMS
   !
!"# " $!
GROUP 14 GUIDED MISSILES
Class 1410 Guided Missile
Systems, Complete
 14   
  ( ")
5677 1410 689:;<9 = 8>7?=@978=9 7=7:9?< (8>?B5987<)
MODERNIZATION OF VOLGA AND PECHORA
AIR DEFENSE MISSILE SYSTEMS
The modernization is intended to:
- extend service life by replacing outdated analog
equipment with up-to-date digital equipment intended
for signal processing, determining target and missile
coordinates, generation of control commands, and
combat crew training;
- reduce the operating costs;
- improve performance characteristics by using of dig-
ital data processing and control algorithms and intro-
ducing additional digital devices;
- provide on-site combat crew retraining.
This modernization improves the cost-effectiveness
ratio.
The design documentation developed for modernized
air defense missile systems (Pechora-2A and Volga-2A)
provides for the use of unified digital equipment
devised on the basis of the engineering solutions incor-
porated in the S-300PMU1 air defense missile system.
Basic Characteristics
Volga Volga-2A
Target engagement
envelope:
altitude range, km 0.1 - 30 0.1 - 30
maximum range, km:
at 0.5-km altitude 24 27
at 5 - 25-km altitude 40 - 55 45 - 60
at 30-km altitude 50 55
maximum cross-range, km:
at 0.5-km altitude 22 26
at 5 - 25-km altitude 38 - 50 40 - 57
at 30-km altitude 34 45
Single-shot kill probability:
at a range of up to 55 km 0.40 - 0.97 0.56 - 0.98
at a range of 55 - 60 km - 0.41 - 0.98
Automatic target lock-on time, s 8 2.5 - 3
9:;<
: «>"» «»
[95\ ?>]9^;=_6`==:
- B^>]59;=9 7^>8>a b87B5c6:6`== _6 7@9: _6?9;< c7:6-
^9ad9e 6;65>f>a>e 6BB6^6:c^< >g^6g>:8= 7=f;65>a, >B-
^9]959;=h 8>>^]=;6: `95= = ^689:, a<^6g>:8= 8>?6;] cB-
^6a59;=h, :^9;=^>a8= g>9a<i ^67@9:>a = ]^. ;6 7>a^9-
?9;;cj `=k^>acj 6BB6^6:c^c;
- c]9d9a59;=9 b87B5c6:6`== 8>?B5987>a;
- B>a<d9;=9 :68:=8>-:9i;=@978=i i6^68:9^=7:=8 _6 7@9:
^965=_6`== `=k^>a<i 65f>^=:?>a >g^6g>:8= = cB^6a59-
;=h, aa>]6 ]>B>5;=:95\;<i `=k^>a<i c7:^>e7:a;
- >g97B9@9;=9 B9^9B>]f>:>a8= (g9_ 99 7cl97:a9;;>f> =_-
?9;9;=h) g>9a<i ^67@9:>a ;6 ?97:6i b87B5c6:6`==.
^= b:>? ^965=_c9:7h b8>;>?=@9786h `9597>>g^6_;>7:\
?>]9^;=_6`== B> 8^=:9^=j «bkk98:=a;>7:\ - 7:>=?>7:\».
6_^6g>:6;;6h 8>;7:^c8:>^786h ]>8c?9;:6`=h ]5h ?>]9^-
;=_=^>a6;;<i  («9@>^6-2» = «o>5f6-2») g6_=^c9:-
7h ;6 =7B>5\_>a6;== c;=k=`=^>a6;;>e `=k^>a>e 6BB6-
^6:c^<, a<B>5;9;;>e 7 B^=?9;9;=9? :9i;=@978=i ^9d9-
;=e, ^965=_>a6;;<i a ! !-300p1.
@ABCADE FGHGIJEHK@JKIK
«>BLMG» «>BLMG-2»
>;< B>^6q9;=h:
]=6B6_>; a<7>:, 8? 0,1 - 30 0,1 - 30
?687=?65\;6h ]65\;>7:\, 8?:
;6 a<7>:9 0,5 8? 24 27
;6 a<7>:9 5 - 25 8? 40 - 55 45 - 60
;6 a<7>:9 30 8? 50 55
?687=?65\;<e B6^6?9:^, 8?:
;6 a<7>:9 0,5 8? 22 26
;6 a<7>:9 5 - 25 8? 38 - 50 40 - 57
;6 a<7>:9 30 8? 34 45
o9^>h:;>7:\ B>^6q9;=h
`95= >];>e ^689:>e:
;6 ]65\;>7:= ]> 55 8? 0,40 - 0,97 0,56 - 0,98
;6 ]65\;>7:= 55 - 60 8? - 0,41 - 0,98
o^9?h 6a:>?6:=@978>f>
_6ia6:6 `95= ;6 !, 7 8 2,5 - 3
592
PART 4  4
MEDIUM-RANGE AIR DEFENSE
MISSILE SYSTEMS
   !
!"# " $!
Basic Characteristics
Pechora Pechora-2A
Target engagement
envelope:
altitude range, km 0.02 - 18 0.02 - 20
maximum range, km:
at 0.5-km altitude 18 23
at 6-km altitude 22 28
at 14 - 20-km altitude 25 28
maximum cross-range, km 16 24
Single-shot kill probability:
at a range of up to 25 km > 0.50 0.72 - 0.99
at a range of 25 - 28 km - 0.51 - 0.99
Automatic target
lock-on time, s 8 2.5 - 3
When modernizing the Pechora air defense missile sys-
tem, 44 analog units are replaced by six digital units.
When modernizing the Volga air defense missile sys-
tem, 78 analog units are replaced by 12 digital units. In
this case, the duration of the system’s maintenance
operations is reduced 2-2.5 times. The modernization
package can be specified at customer request.
@ABCADE FGHGIJEHK@JKIK
«ENBHG» «ENBHG-2»
>;< B>^6q9;=h:
]=6B6_>; a<7>:, 8? 0,02 - 18 0,02 - 20
?687=?65\;6h ]65\;>7:\, 8?:
;6 a<7>:9 0,5 8? 18 23
;6 a<7>:9 6 8? 22 28
;6 a<7>:9 14 - 20 8? 25 28
?687=?65\;<e B6^6?9:^, 8? 16 24
a9^>h:;>7:\ B>^6q9;=h
`95= >];>e ^689:>e:
;6 ]65\;>7:= ]> 25 8? ;9 g>599 0,50 0,72 - 0,99
;6 ]65\;>7:= 25 - 28 8? - 0,51 - 0,99
o^9?h 6a:>?6:=@978>f>
_6ia6:6 `95= ;6 !, 7 8 2,5 - 3
GROUP 14 GUIDED MISSILES
Class 1410 Guided Missile
Systems, Complete
 14   
  ( ")
5677 1410 689:;<9 = 8>7?=@978=9 7=7:9?< (8>?B5987<)
^= ?>]9^;=_6`==  «9@>^6» 44 6;65>f>a<i g5>86 _6-
?9;hj:7h 6 `=k^>a<?= g5>86?=. ^= ?>]9^;=_6`== 
«o>5f6» 78 6;65>f>a<i g5>86 _6?9;hj:7h 12 `=k^>a<?=
g5>86?=. ^>]>5q=:95\;>7:\ ^6g>: B> :9i;=@978>?c >g75c-
q=a6;=j 8>?B5987>a B^= b:>? 7>8^6l69:7h a 2-2,5 ^6_6.
gu9? = ;6B^6a59;=9 ?>]9^;=_6`== ?>fc: c:>@;h:\7h B>
q956;=j _686_@=86.
593
PART 4  4
MEDIUM-RANGE AIR DEFENSE
MISSILE SYSTEMS
   !
!"# " $!
GROUP 14 GUIDED MISSILES
Class 1410 Guided Missile
Systems, Complete
 14   
  ( ")
6788 1410 79:;<=: > 9?8@>A:89>: 8>8;:@= (9?@C6:98=)
$%&'
% «&$» («*»)
E:6F @?G:H<>I7J>>: C?L=M:<>: ?N<:L?O CH?>IL?G>-
;:6F<?8;>, H78M>H:<>: NH7<>J P?:L?N? CH>@:<:<>Q
> C7H97 C?H7R7:@=S J:6:O ?; L:H;?6:;?L, L ;?@ A>8-
6: I7L>87TU>S, 87@?6:;?L ;79;>A:89?O > 8;H7;:N>-
A:89?O 7L>7J>> G? ;79;>A:89>S P766>8;>A:89>S >
7L>7J>?<<=S 9H=67;=S H79:;, C?L=M:<>: C?@:S?I7-
U>U:<<?8;>.
W?IH?8M>: P?:L=: L?I@?R<?8;> G?8;>N<X;= I7 8A:;:
- LL:G:<>Q L 8?8;7L  «L7GH7;» [6:@:<;?L 
«\X9-1-2» 8 G?H7P?;9?O >S G6Q 8?CHQR:<>Q 8? 8H:G-
8;L7@>  «L7GH7;»;
- @?G:H<>I7J>> !_ 1!912(1): LL:G:<>: J>`-
H?L=S 8>8;:@ !"E, H78C?I<7L7<>: 967887 J:6:O,
H78M>H:<>: G>7C7I?<7 A78;?; 97<767 C?G8L:;7, I7-
@:<7 X8>6>;:6:O !Wa <7 67@C7S P:NXU:O L?6<= <7
;L:HG?;:6F<=: ;H7<I>8;?H<=: X8>6>;:6>, LL:G:<>:
;:6:9?G?L?N? 97<767 8LQI> 8 9?@7<G<=@ CX<9;?@ XC-
H7L6:<>Q;
- I7@:<= 8H:G8;L XCH7L6:<>Q (\_-E) > 8;7H?N?
C7H97 H7G>?6?97J>?<<=S 8;7<J>O <7 @?G:H<>I>H?L7<-
<=: > <?L=:  ! 8 >8C?6FI?L7<>:@ 9?@7<G<?N? CX<9-
;7 9?@C6:987 «\X9-1-2» 9!4701-2 > CX<9;7 ?PH7-
P?;9> H7G>?6?97J>?<<?O ><`?H@7J>> -2W.
W=M:C:H:A>86:<<=: @?G:H<>I7J>> 8H:G8;L
9?@C6:987 C?IL?6Q; ?HN7<>I?L7;F GL: 8;HX9;XH=
MODERNIZED KVADRAT (KUB)
AIR DEFENSE MISSILE SYSTEM
The modernization is intended to enhance the system’s
fire power potential, expand target engagement
envelope and range of potential targets (helicopters,
including hovering ones, tactical and strategic aircraft,
tactical ballistic and air-launched cruise missiles), as well
as to increase the system’s jamming immunity.
The enhanced combat performance characteristics are
achieved owing to:
- introduction of the Buk-M1-2 AD missile system compo-
nents into the Kvadrat AD missile system complement after
their modification to interface with the Kvadrat ADMS;
- modernization of the 1S91M2(M1) control, reconnais-
sance and guidance system (CRGS): introduction of
digital moving target descrimination systems, discrimi-
nation of target classes, extension of the illumination
channel frequency range, replacement of microwave
amplifiers built around traveling wave tubes by solid-
state transistor amplifiers, as well as introduction of a
coded telemetry channel to maintain communication
with the command/control post;
- replacement of command/control assets and an out-
dated pool of radar stations by modernized and new-
generation radars with the use of the 9S470M1-2 com-
mand post of the Buk-M1-2 AD missile system and the
PORI-P2VM radar data processing post.
594
PART 4  4
MEDIUM-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=)
The aforementioned modernization of the system
assets makes it possible to establish two options of
interaction of missile battery combat assets and com-
mand/control posts of the Kvadrat AD missile system.
First Option
Six organic missile batteries with the modernized
1S9M1 (M2) CRGSs are controlled over new coded
telemetry communications lines from the modernized
9S470M1-2 command post of the Buk-M1-2 AD missile
system, which receives radar data via the PORI-P2VM
post from the modernized P-18 and P-19 radars,
9S18M1-1 radar of the Buk-M1-2 AD missile system
and an organic PRV altimeter.
?HN7<>I7J>> LI7>@?G:O8;L>Q P?:L=S 8H:G8;L H7-
9:;<=S P7;7H:O > 9?@7<G<=S CX<9;?L P?:L?N? XC-
H7L6:<>Q  «L7GH7;».
9:;<= ;>:?>@A
y:8;F M;7;<=S P7;7H:O 8 @?G:H<>I>H?L7<<=@> !_
1!91(2) XCH7L6QT;8Q C? <?L=@ 6><>Q@ ;:6:9?G?L?O
8LQI> ?; G?H7P?;7<<?N? 9?@7<G<?N? CX<9;7 9!4701-2
 «\X9-1-2», CH><>@7TU:N? H7G>?6?97J>?<<XT ><-
`?H@7J>T A:H:I -2W ?; @?G:H<>I>H?L7<<=S
 ! -18 > -19, ?;  ! 9!181-1  «\X9-1-2» >
M;7;<?N? L=8?;?@:H7 (W).

CP
C
TAR

SPM
%
LL

SPL
%
LL

SPL
%
LL

SPL

SPL

SPL

SPL

SPL

SPL

SPL

SPM

CRGS

SPM

CRGS

CRGS

CRGS

CRGS

CRGS

CRGS

CRGS

CRGS
-2&
PORI-P2VM

CP
C
TAR
 ! «:P?-!W»
 ! «78;7-22»
W
Nebo-SV radar
Kasta-2E2 radar
PRV altimeter
 ! «:P?-!W»
 ! «78;7-22»
W
Nebo-SV radar
Kasta-2E2 radar
PRV altimeter
-2&
PORI-P2VM
9:;<= ;>:?>@A
First option
&AF:F= ;>:?>@A
Second option
595
PART 4  4
MEDIUM-RANGE AIR DEFENSE
MISSILE SYSTEMS
   !
!"# " $!
Second Option
Three organic missile batteries with modernized
1S91M1(M2) CRGSs are controlled over new coded
telemetry communications lines from a modernized
9S470M1-2 CP, while three batteries (each comprising
one 9A310M1-2 SPM and one 9A39M1 LL) are controlled
via standard telemetry communications lines (9S624 -
9S625) from the 9S470M1-2 CP, which receives radar
data via the PORI-P2VM post from new-generation Nebo-
SV and Kasta-2E2 radars or modernized P-18 and P-19
radars, 9S18M1 TAR and an organic PRV altimeter.
GROUP 14 GUIDED MISSILES
Class 1410 Guided Missile
Systems, Complete
 14   
  ( ")
6788 1410 79:;<=: > 9?8@>A:89>: 8>8;:@= (9?@C6:98=)
&AF:F= ;>:?>@A
H> M;7;<=: P7;7H:> 8 @?G:H<>I>H?L7<<=@> !_
1!911(2) XCH7L6QT;8Q C? <?L=@ 6><>Q@ ;:6:9?G?-
L?O 8LQI> ?; G?H7P?;7<<?N? 9?@7<G<?N? CX<9;7
9!4701-2, 7 ;H> P7;7H:> (L 8?8;7L: 97RG?O ?G<7 !_
93101-2 > ?G<7 _ 9391) XCH7L6QT;8Q C? M;7;-
<?O 6><>> !! (9!624 - 9!625) ?;  9!4701-2, CH>-
<>@7TU:N? H7G>?6?97J>?<<XT ><`?H@7J>T A:H:I
-2W ?; <?L=S  ! «:P?-!W»,  ! «78;7-
22» >6> @?G:H<>I>H?L7<<=S  ! -18, -19, !E
9!181 > M;7;<?N? W.
J@F;@<9 K>:>LA9:?JA?L?
 ?G:H<>I>H?L7<<=O 
G? @?G:H<>I7J>> 8 _ 393 8  «\X9-1-2»
>C= C?H7R7:@=S J:6:O 87@?6:;= ,
L:H;?6:;=
7H7@:;H= C? G76F<?8;> 4-25 4-25 3-42
I?<= C? L=8?;: 0,1-7(G? 14 8 -1) 0,03-14 0,015-25 / 2-10
C?H7R:<>Q, C? 9XH8?L?@X
9@ C7H7@:;HX G? 18 G? 18 G? 25
"76F<?8;F 8;H:6FP=
C? <7GL?G<?O J:6>, 9@ G? 18-25
Ma98. 89?H?8;F C?H7R7:@=S
J:6:O, @/8 G? 600 G? 600 G? 1200
W:H?Q;<?8;F 87@?6:;= G? 0,8 G? 0,9 0,9 - 0,95
C?H7R:<>Q \ - - 0,5 - 0,6
?G<?O  - 0,3-0,4 0,6 - 0,7
_ L:H;?6:;= G? 0,3 0,45 0,7 - 0,8
!C?8?P <7L:G:<>Q _
C?6X79;>L<?: 87@?<7L:G:<>: C?6X79;>L<?: 87@?<7L:-
G:<>: 8 H7G>?9?HH:9J>:O
?6>A:8;L? _ <7 !_,
!_/_ 3 3 4 / 8
7887 P?:L?O A78;> _, 9N 57 57 70
WH:@Q H:79J>>, 8 22-24 22-24 20
87@?6:;=  > !,
;79;>A:89>: P766>-
8;>A:89>:, 9H=67;=:
> 7L>7J>?<<=: H79:-
;=, L:H;?6:;=, " ,
<7GL?G<=: J:6>
87@?6:;=  > !,
9H=67;=: H79:;=
> L:H;?6:;=
Basic Characteristics
AD
missile system
Modernized AD
missile system
before modernization
with 3M9M3 with Buk-M1-2
»
Types of engaged Tactical aircraft,
targets helicopters
Kill range
4 - 25 4 - 25 3 - 42
zone altitude
0.1-7 (up to 14 with -1)
0.03-14 0.015-25 / 2-10
parameters,
km cross-range
up to 18 up to 18 up to 25
Waterborne target
engagement range, km
up to 18-25
Target speed, m/s
up to 600 up to 600 up to 1200
Single-shot aircraft
up to 0.8 up to 0.9 0.9 - 0.95
kill TBM
- - 0.5 - 0.6
probability CM
- 0.3-0.4 0.6 - 0.7
helicopters
up to 0.3 0.45 0.7 - 0.8
Guidance semi-active homing radio-command
corrected semi-
active homing
Number of ADMs
on SPLV/LL
334 / 8
Weight of ADM warhead, kg
57 57 70
Response time, s
22 - 24 22 - 24 20
Tactical and strate-
gic aircraft, tactical
ballistic, cruise and
airborne missiles,
helicopters, RPV,
surface targets
Tactical and
strategic aircraft,
cruise missiles
and helicopters
596
PART 4  4
SHORT-RANGE
AIR DEFENSE MISSILE
AND GUN-MISSILE SYSTEMS
 
- !"# $ %&
$%' (%)&
GROUP 14 GUIDED MISSILES
Class 1410 Guided Missile
Systems, Complete
 14   
  ( ")
;<== 1410 <>?@AB? C >D=ECF?=>C? =C=@?EB (>DEH;?>=B)
TOR-M1 AUTONOMOUS GROUND FORCES
AIR DEFENSE MISSILE SYSTEM
Intended for effective defense of troops, civilian and
industrial facilities from current and future air attack
weapons, primarily high-precision weapons, as well as
from aircraft, helicopters, cruise missiles, guided aerial
bombs and remotely piloted vehicles.
The system incorporates the following main components:
The 9A331-1 combat vehicle
The basic component of the system is a combat vehi-
cle mounted on a cross-country tracked chassis in the
intermediate weight category. The combat vehicle can
6 7 6867 97
7   «- 1»
V?WA<XA<F?A< W;Y Z[[?>@C\AD]D HVC>VB@CY \D^=>, ]V<-
_W<A=>C` C HVDEBa;?AAB` Dbc?>@D\ D@ =D\V?E?AAB` C
H?V=H?>@C\AB` =V?W=@\ \DXWdaAD]D A<H<W?ACY, HV?_W?
\=?]D \B=D>D@DFAD]D DVd_CY, < @<>_? =<ED;?@D\, \?V@D;?-
@D\, >VB;<@B` V<>?@, dHV<\;Y?EB` <\C<bDEb C WC=@<AeC-
DAAD HC;D@CVd?EB` ;?@<@?;fAB` <HH<V<@D\.
<=>?@A B@CDE@ 9331-1
=AD\ABE Z;?E?A@DE =C=@?EB Y\;Y?@=Y bD?\<Y E<aCA<,
=EDA@CVD\<AA<Y \ b<XD\DE \<VC<A@? A< \B=D>DHVD`DWC-
EDE ]d=?ACFADE a<==C HVDE?_d@DFAD^ \?=D\D^ ><@?]D-
597
PART 4  4
SHORT-RANGE
AIR DEFENSE MISSILE
AND GUN-MISSILE SYSTEMS
 
- !"# $ %&
$%' (%)&
GROUP 14 GUIDED MISSILES
Class 1410 Guided Missile
Systems, Complete
 14   
  ( ")
;<== 1410 <>?@AB? C >D=ECF?=>C? =C=@?EB (>DEH;?>=B)
detect aerial targets on the move and launch air
defense missiles at two highest-threat targets from a
short halt.
The combat vehicle comprises:
- self-propelled armored tracked chassis;
- three-dimensional target acquisition radar;
- digital computer;
- antenna stabilization system;
- ground-based IFF interrogator;
- target tracking phased-array radar;
- TV/optical sight;
- automatic launch equipment;
- coded telemetry and command radio communication-
s system;
- navigation, survey and orientation equipment;
- primary power supply system;
- crew life-support equipment;
- auxiliary equipment.
The 9M334 air defense missile module
(9M331 missile and 9Ya281 transport launch canister)
The missile is designed around a canard configuration.
It is launched vertically by a powder catapult to a
height of 15 - 20 m. It is then tilted in the target direc-
tion and its main solid-propellant rocket motor gets
ignited.
The single-stage rocket motor has two operating
modes. In the liftoff mode, the motor imparts the
maximum speed of 850 m/s to the missile for 4 s of
VCC. b?=H?FC\<?@ DbA<Vd_?AC? \DXWdaAB` e?;?^ \ W\C-
_?ACC C Hd=>C X?AC@AD-dHV<\;Y?EB` V<>?@ HD W\dE A<C-
bD;?? DH<=ABE e?;YE = >DVD@>D^ D=@<AD\>C.
&D=@<\ bD?\D^ E<aCAB:
- ]d=?ACFAD? =<ED`DWAD? bVDACVD\<AAD? a<==C;
- @V?`>DDVWCA<@A<Y V<WCD;D><eCDAA<Y =@<AeCY DbA<Vd_?-
ACY e?;?^ (&p);
- eC[VD\<Y \BFC=;C@?;fA<Y E<aCA<;
- =C=@?E< =@<bC;CX<eCC <A@?AAB (&&);
- A<X?EAB^ V<WCDX<HVD=FC>;
- V<WCD;D><eCDAA<Y =@<AeCY =DHVD\D_W?ACY e?;?^ = [<-
XCVD\<AAD^ V?a?@>D^;
- @?;?\CXCDAAD-DH@CF?=>C^ \CXCV (q);
- <HH<V<@dV< =@<V@D\D^ <\@DE<@C>C (&);
- =C=@?E< @?;?>DWD\D^ C DH?V<@C\AD->DE<AWAD^ V<WCD-
=\YXC;
- <HH<V<@dV< A<\C]<eCC, @DHDHVC\YX>C C DVC?A@CVD\<ACY
();
- =C=@?E< H?V\CFAD]D Z;?>@VDHC@<ACY;
- <HH<V<@dV< _CXA?Db?=H?F?ACY Z>CH<_<;
- \=HDED]<@?;fA<Y <HH<V<@dV<.
9>EDOEPQ R@S>OEPQ B=TUVW 9 334
(R@S>O@ 9 331,  97281)
<>?@< \BHD;A?A< HD =`?E? «d@><», =@<V@d?@ \?V@C><;fAD
= HDEDtfu HDVD`D\D^ ><@<Hd;f@B A< \B=D@d 15 - 20 E?@-
VD\, X<@?E HVDC=`DWC@ ?? =>;DA?AC? \ =@DVDAd e?;C C
\>;uF?AC? D=AD\AD]D @\?VWD@DH;C\AD]D W\C]<@?;Y.
(\C]<@?;f V<>?@B DWAD=@dH?AF<@B^, W\d`V?_CEAB^. q
  • 2008 — 2025 «СтудМед»