Каталог - Оружие России 2000 c82-795
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PART 2 2
GROUP 13 AMMUNITION
AND EXPLOSIVES
Class 1325 Bombs
13 !", $" ! %
! $&"$" $ ' $
1325
422
AIR BOMBS #$%$&''() *&+*(
()*+),- ./0/12-03(2313
,-., 450
,, 2500
+, 12 500
3- *4 1- 126
Basic Characteristics
Diameter, mm 450
Length, mm 2,500
Weight, kg 500
Number of submunitions 126
()*+),- ./0/12-03(2313
,-., 450
,, 2500
+, 12 480
3- *4 1- 10
Basic Characteristics
Diameter, mm 450
Length, mm 2,500
Weight, kg 480
Number of submunitions 10
500-kg SIZE RBK-500U OAB-2.5RT
UNIFIED CLIUSTER BOMB LOADED
WITH FRAGMENTATION
SUBMUNITIONS
This bomb is intended to engage easily vulnerable
materiel as well as entrenched and unsheltered man-
power, with submunitions exploding in the air.
It is dropped from altitudes of 100 to 20,000 m at a
speed of 500 to 2,000 km/h.
I!J!K!$IIL &$L M$L
% %N! 500 1O $ ILP I!!
%NI"M! $"M! QN M IM!
%-500 -2,5
P.QR3 QS T.US 21VSRW -X1
UW , XQSYWS 1TX, -.ZSX -1.-
-X V3-1X --. &T3- QT.X-W
TQ. X [-.
P.S-S - 100 - 20000 T. 1.-SX 500 -
2000 1/3.
500-kg SIZE RBK-500U BETAB-M
UNIFIED CLUSTER BOMB LOADED
WITH CONCRETE-PIERCING SUBMUNITIONS
This bomb is intended to damage runways and main
taxiways on all types of modern airfields.
It is dropped from altitudes of 300 to 5,000 m at a
speed of 500 to 1,200 km/h.
I!J!K!$IIL &$L M$L %
%N! 500 1O $ ILP I!! IRI"M!
$"M! QN M IM! %-500 -M
P.QR3 QS T.US R--TQ3X T
2-.\X .VUX Q.U1 X -T .-
X [.Q..
P.S-S - 300 - 5000 T. 1.-SX 500 -
1200 1/3.
PART 2 2
GROUP 13 AMMUNITION
AND EXPLOSIVES
Class 1325 Bombs
13 !", $" ! %
! $&"$" $ ' $
1325
423
AIR BOMBS #$%$&''() *&+*(
500-kg SIZE RBK-500U OFAB-50UD
UNIFIED CLUSTER BOMB LOADED
WITH HIGH EXPLOSIVE FRAGMENTATION
BOMBLETS
This bomb is intended to engage lightly armored and
easily vulnerable materiel, manpower, ammunition
dumps, field fortifications, military industrial facilities
and communications lines.
It ensures two types of effect on the target (depending
on setting): above-surface or penetrating.
It is dropped from altitudes of 180 to 20,000 m at a
speed of 500 to 2,000 km/h.
4!5!6!$447 &$7 8$7
% %9! 500 :; $ 47< 4!!
%94-54"8! $!88!
%-500 5-50=
FGHIJ HK LGMK NOGGP
NOQKIP RSO, MP , LS OH
LGL, POS TGRTOS GQMP,
-LGUS VOR OQOP.
&LJR 2 H HPRK L ( IR R
LGIHP QRO): HLGSR LG-
OWX.
FGKRK R 180 - 20000 LG OGRKS 500 -
2000 O/J.
>?@A?BC DEFE:GCFH>GH:H
YRG, 450
Y, 2500
+, ON 520
JR OR 10
Basic Characteristics
Diameter, mm 450
Length, mm 2,500
Weight, kg 520
Number of bomblets 10
>?@A?BC DEFE:GCFH>GH:H
YRG, 450
Y, 2500
+, ON 520
JR *^ OR 352
Basic Characteristics
Diameter, mm 450
Length, mm 2,500
Weight, kg 520
Number of submunitions 352
500-kg SIZE RBK-500U-PTAB
UNIFIED CLUSTER BOMB
LOADED WITH HEAT SUBMUNITIONS
This bomb is intended to defeat tanks, infantry combat
vehicles, APCs, SP artillery mounts and other armored
materiel in combat formations, concentration areas and
on the march.
It is dropped from altitudes of 80 to 20,000 m at a
speed of 500 to 2,000 km/h.
4!5!6!$447 &$7 8$7
% %9! 500 :; $ 47< 4!!
!$4%$"8! %897!$4"8!
$"8! Q9 8 48! %-500
FGHIJ HK LGMK RO, *+F, *`a, bc
HGQNP GGP RSO, SHKXPK -
S LGKHOS, RS GHRJK GU.
FGKRK R 80 - 20000 LG OGRKS 500
- 2000 O/J.
424
AIR BOMBS
GROUP 13 AMMUNITION
AND EXPLOSIVES
Class 1325 Bombs
13 , !" #"
$ !" %"
!"" 1325 #$!%$&''() *&+*(
PART 2 !"' 2
M6 AND M6T SMALL-SIZE TARGET
The target is designed to train Air Defense and Air
Force personnel in detecting and engaging air targets.
The target is an air bomb which simulates an air target
in the passive radar and IR bands. The design of the
M6T target and its container incorporates modern cor-
rosion-resistant coatings, composite materials and
sealants, reliable packings, as well as modern methods
of checkouts and testing, which allows its storage and
use in any climates, including the tropics.
+,"-. +/-' +6, +6"
CD)E'!F'!G)'! E H &*IG)'$H $G'&J& "&"K!#! C L
&*'!DIM)'$N $ O&D!M)'$N #&FEIP'(Q %) )R.
$P)'S OD)E"K!# H)K "&*&R !#$!*&+*I, $+$K$DINTIN
#&FEIP'IN %) S # O!""$#'&+ D!E$& &U!%$&''&+ $ K)O &-
#&+ E$!O!F&'!Q.
U&'"KDIU%$$ +$P)'$ 6V $ K!D( $"O& SF&#!'( "&#D)-
+)''() !'K$U&DD&F$&''() O&UD(K$H, U&+*$'$D&#!''()
+!K)D$! ( $ J)D+)K$U$, '!E)M'() IO &K'$K) $, ! K!UM)
"&#D)+)''() +)K&E( U&'KD& S'(Q OD&#)D&U $ $"O(K!'$R,
GK& O&F#& H)K &*)"O)G$KS )) QD!')'$) $ OD$+)')'$) #
N*(Q U $+!K$G)"U$Q F&'!Q, # K&+ G$" ) $ # KD&O$G)"U&+
U $+!K).
0123145 67879:58;0:;9;
W$!+)KD, ++ 280
W $'!, ++ 1065
Z!F+!Q "K!*$ $F!K&D!, ++ 345
!""!, UJ 98
Z)M$+( OD$+)')'$H:
#("&K!, + 2500 - 17 000
"U&D&"KS ($"K$''!H), U+/G 750 - 1200
#D)+H J&D)'$H a!U) !, " ') +)')) 195
"$ ! "#)K!, UE ') +)')) 2
E! S'&"KS '!* NE)'$H, U+ E& 35
Basic Characteristics
Diameter, mm 280
Length, mm 1,065
Fin span, mm 345
Weight, kg 98
Application modes:
altitude, m 2,500 - 17,000
speed (true), km/h 750 - 1,200
flare burning time, s at least 195
light intensity, Mcd at least 2
observer-target range, km up to 35
P-50T THERMOSTABLE
PRACTICE BOMB
This bomb is designed to train flying personnel in
bombing. It can be used at any time of day or night and
is dropped from altitudes of 200 to 25,000 m at a
speed of 500 to 2,500 km/h.
"+"I#. #"!#.
J--. + -50"
CD)E'!F'!G)'! E H &*IG)'$H )K'&J& "&"K!#! *&+*&+)K!-
'$N.
&M)K $"O& SF&#!KS"H # N*&) #D)+H "IK&U.
CD$+)'H)K"H " #("&K 200 - 25000 + OD$ "U&D&"KHQ 500 -
2500 U+/G.
0123145 67879:58;0:;9;
W$!+)KD, ++ 203
W $'!, ++ 1044
!""!, UJ 50
D)+H #$E$+&"K$ "$J'! !, ":
"#)K&#&J& 16
E(+&#&J& 35
Basic Characteristics
Diameter, mm 203
Length, mm 1,044
Weight, kg 50
Signal visibility time, s:
light 16
smoke 35
425
PART 2 2
UNGUIDED
AIRCRAFT ROCKETS
!"
GROUP 13 AMMUNITION
AND EXPLOSIVES
Class 1340 Rockets, Rocket Ammunition and Rocket Components
13 !", $" ! %
! $&"$" $ ' $
!5677 1340 89:;6<5=8>?8 ;6@8A?, BC DE8<E8 E7F6G8FB8 B 7E7A6<F?8 H67AB
S-8 UNGUIDED
AIRCRAFT ROCKETS
These rockets are intended to engage all kinds of ground
targets and are the main type of ammunition for combat
helicopters
- $./ 0" $!1!--"
% " ! 0" -8
;8OF6PF6H8F? O5= :E;6Q8FB= F6P8>F?C R858S 5TDEUE <BO6 B
=<5=TA7= E7FE<F?> <BOE> DE8:;B:67E< DE8<?C <8;AE58AE<.
WB7A8>6 W-8 - E7FE<FES @65BD; < @56778 F89:;6<5=8>EUE
C-80
S-8BM
-80
S-8PM
-830
S-8DM
-810
S-8TsM
-8-0
S-8-OM
-8
S-8
-835
S-8DF
-8%0
S-8%0
- $./ 0" $!1!--" % "
-$- -&- -!/
;8OF6PF6H8F? O5= :E;6Q8FB= EOBFEHF?C >65E;6P>8;F?C
R858S (:;EHF?C, D;EFB;E<6FF?C, 58U@E9=P<B>?C) B QB<ES
7B5? :;EAB<FB@6. 858<E8 F6PF6H8FB8 E:;8O85=8A7=
<BOE> :E;6Q6TG8UE O8S7A<B= 88 DE8<ES H67AB (\]).
6 <EE;9Q8FBB W ^ 7E7AE=A @65BD;E< 80, 122,
240 B 266 >>, B>8TGB8 7EEA<8A7A<9TGB8 F6B>8FE<6FB=:
W-8, W-13, W-24 B W-25.
75E<F?8 F6B>8FE<6FB= ;6@8A 7EO8;Q6A 7<8O8FB= E AB:6C
\] < <BO8 BFO8@7E<. 6:;B>8;, W-8! - @65BD;6
80 >> 7 \] @9>95=AB<FE-E7@E5EHFEUE O8S7A<B=,
W-25- ^ - 7 \] E7@E5EHFE-a9U67FEUE O8S7A<B= B A. O.
MAIN-PURPOSE
ROCKETS
Main-purpose rockets are designed to engage single
small targets (soft, hard, armored) and enemy
manpower. The purpose of a rocket is dictated by the
destructive effect of the warhead.
The rockets operational with the Russian Air Force have
calibers of 80, 122, 240 and 266 mm and are respec-
tively designated S-8, S-13, S-24 and S-25.
The rocket designation has letters indicating the
warhead type. For example, S-8KO means an 80mm
rocket with HEAT fragmentation warhead, while S-25-
OF implies a rocket with HE fragmentation warhead,
etc.
426
PART 2 2
UNGUIDED
AIRCRAFT ROCKETS
!"
GROUP 13 AMMUNITION
AND EXPLOSIVES
Class 1340 Rockets, Rocket Ammunition and Rocket Components
13 !", $" ! %
! $&"$" $ ' $
!5677 1340 89:;6<5=8>?8 ;6@8A?, BC DE8<E8 E7F6G8FB8 B 7E7A6<F?8 H67AB
S-8KOM
This rocket is intended to engage modern tanks, lightly
armored and soft-skinned combat materiel. Owing to
the fragmentation effect, the rocket also inflicts dam-
age on manpower.
Basic Characteristics
Caliber, mm 80
Length, mm 1,570
Weight, kg:
rocket 11.3
warhead 3.6
explosive 0.9
Armor penetration, mm 400
Firing range, m 1,300 - 4,000
Rocket velocity, m/s 610
Operating temperature range,
o
C ±60
S-8BM
This rocket is intended to engage materiel and man-
power in fortifications. A specially designed warhead
pierces the reinforced concrete barrier and explodes
on penetration, forming a large number of splinters.
Basic Characteristics
Caliber, mm 80
Length, mm 1,540
Weight, kg:
rocket 15.2
warhead 7.41
explosive 0.6
Reinforced concrete penetration, mm 800
Firing range, m 1,200 - 2,200
Rocket velocity, m/s 450
Operating temperature range,
o
C ±60
-8%0
;8OF6PF6H8F6 O5= :E;6Q8FB= 7E<;8>8FF?C A6F@E<, 58U-
@ED;EFB;E<6FFES B F8D;EFB;E<6FFES DE8<ES A8CFB@B.
\56UEO6;= E7@E5EHFE>9 O8S7A<BT ;6@8A6 :E;6Q68A B QB-
<9T 7B59.
=>?@>AB CDEDFGBEH=GHFH
!65BD;, >> 80
m5BF6, >> 1570
6776, @U:
;6@8A? 11,3
DE8<ES H67AB 3,6
0,9
"E5GBF6 :;EDB<68>ES D;EFB, >> 400
m65nFE7An :97@6, > 1300 - 4000
W@E;E7An ;6@8A?, >/7 610
"8>:8;6A9;F?S OB6:6PEF :;B>8F8FB=, U;6O. W ±60
-80
;8OF6PF6H8F6 O5= :E;6Q8FB= >6A8;B65nFES H67AB B QB-
<ES 7B5? < aE;ABaB@6RBEFF?C 7EE;9Q8FB=C. W:8RB65nFE
7@EF7A;9B;E<6FF6= DE8<6= H67An ;6@8A? :;EDB<68A Q858-
PED8AEFF9T :;8U;6O9 B <P;?<68A7=, ED;6P9= DE5noE8 @E-
5BH87A<E :E;6Q6TGBC E7@E5@E<.
=>?@>AB CDEDFGBEH=GHFH
!65BD;, >> 80
m5BF6, >> 1540
6776, @U:
;6@8A? 15,2
DE8<ES H67AB 7,41
0,6
"E5GBF6 :;EDB<68>EUE Q858PED8AEF6, >> 800
m65nFE7An :97@6, >> 1200 - 2200
W@E;E7An ;6@8A?, >/7 450
"8>:8;6A9;F?S OB6:6PEF :;B>8F8FB=, U;6O. W ±60
6<B6RBEFFEUE ;6@8AFEUE <EE;9Q8FB= (), ;8o68A 76>?8
;6PFEED;6PF?8 P6O6HB, 7AE=GB8 :8;8O 6<B6RB8S.
6@8AF?S O<BU6A85n - F6 A<8;OE> AE:5B<8, 79>>6;F?S B>:95n7
A=UB 5800 F7 B <;8>= ;6DEA? 0,7 7. 8UE @EF7A;9@RBB B7:E5n-
P9TA7= :;EU;877B<F?8 >8AEO? aE;>EED;6PE<6FB= @E;:976 BP
UEAE<EUE 65T>BFB8<EUE :;E@6A6, E;BUBF65nF?8 A8CFBH87@B8
;8o8FB= :E EAO85nF?> p58>8FA6>, F6:;6<58FF?8 F6 7FBQ8FB8
A;9OE8>@E7AB BPUEAE<58FB= O<BU6A85= B 8UE 7AEB>E7AB.
F67AE=G88 <;8>= F6 <EE;9Q8FBB 7E7AE=A 758O9TGB8 AB:?
;6@8A W-8:
- W-8! - 7 @9>95=AB<FE-E7@E5EHFES DE8<ES H67AnT (\]);
- W-8\ - 7 D8AEFEDESFES (:;EFB@6TG8S) E7@E5EHFE-
a9U67FES \];
- W-8m - 7 \], 7F6;=Q8FFES EDr8>FE-O8AEFB;9TG8S 7>87nT;
- W-8" - 7 A6FO8>FES @9>95=AB<FE-E7@E5EHFES \];
- W-8m^ - 7 a9U67FES \], 7F6;=Q8FFES EDr8>FE-
O8AEFB;9TG8S 7>87nT;
- W-8- - 7 E7<8ABA85nFES \];
- W-8 - 7 \], 7F6;=Q8FFES OB:E5nF?>B EA;6Q6A85=>B;
- W-8 - 7 R8589@6P6A85nFES UE5E<FES H67AnT.
The S-8 system is the main caliber weapon in the class of
unguided aircraft rockets and can solve a variety of aircraft
missions.
The rocket is provided with a solid propellant motor with a
summary thrust pulse of 5,800 N.s and operating time of
0.7 s. Progressive methods for body shaping from ready-
made rolled aluminum and unique engineering solutions in
terms of separate elements aimed at reducing motor man-
ufacturing labor consumption and costs are used in its con-
struction.
The following types of S-8 rockets are operational today:
- S-8KOM with HEAT fragmentation warhead;
- S-8BM with concrete-piercing (penetrating) HE fragmen-
tation warhead;
- S-8DM with fuel-air explosive warhead;
- S-8T with tandem HEAT fragmentation warhead;
- S-8DF with fuel-air explosive warhead;
- S-8-OM with illuminating warhead;
- S-8PM with chaff warhead;
- S-8TsM with target designating warhead.
427
PART 2 2
UNGUIDED
AIRCRAFT ROCKETS
!"
-830
;8OF6PF6H8F6 O5= :E;6Q8FB= ;6P5BHF?C <BOE< R858S,
F6CEO=GBC7= < E@E:6C, A;6Fo8=C, D5BFO6Q6C, ED<65E<6FB-
=C, < 9P@BC :;ECEO6C, < ;E77?:=C @6>F8S, < 7@56O@6C >87A-
FE7AB, :8G8;6C B :;EHBC :EOEDF?C 9@;?AB=C. \E8<6= H67An
;6@8A? 7F6;=Q8F6 EDr8>FE-O8AEFB;9TG8S 7>87nT ( mW).
=>?@>AB CDEDFGBEH=GHFH
!65BD;, >> 80
m5BF6, >> 1700
6776, @U:
;6@8A? 11,6
DE8<ES H67AB 3,8
7>87B 2,15
m65nFE7An :97@6, > 1300 - 4000
";EAB5E<?S p@<B<658FA, @U 5,5 - 6
W@E;E7An ;6@8A?, >/7 590
"8>:8;6A9;F?S OB6:6PEF :;B>8F8FB=, U;6O. W ±60
-8
;8OF6PF6H8F6 O5= :E;6Q8FB= 7E<;8>8FF?C A6F@E<, < AE>
HB758 E7F6G8FF?C p58>8FA6>B OBF6>BH87@ES P6GBA?,
58U@ED;EFB;E<6FFES B F8D;EFB;E<6FFES DE8<ES A8CFB@B.
\56UEO6;= E7@E5EHFE>9 O8S7A<BT ;6@8A6 :E;6Q68A B
QB<9T 7B59.
=>?@>AB CDEDFGBEH=GHFH
!65BD;, >> 80
m5BF6, >> 1680
6776, @U:
;6@8A? 15
DE8<ES H67AB 6,6
1,6
"E5GBF6 :;EDB<68>ES D;EFB, >> 440
m65nFE7An :97@6, > 1300 - 4000
W@E;E7An ;6@8A?, >/7 470
"8>:8;6A9;F?S OB6:6PEF :;B>8F8FB=, U;6O. W ±60
-835
;8OF6PF6H8F6 O5= :E;6Q8FB= QB<ES 7B5? B
58U@E9=P<B>ES A8CFB@B, ;67:E5EQ8FF?C < 7@56O@6C
>87AFE7AB B <ES7@E<?C aE;ABaB@6RBEFF?C 7EE;9Q8FB=C
EA@;?AEUE AB:6.
=>?@>AB CDEDFGBEH=GHFH
!65BD;, >> 80
m5BF6, >> 1680
6776, @U:
;6@8A? 13,4
DE8<ES H67AB 5,5
7F6;=Q8FB= (7>87B) 3,3
";EAB5E<?S p@<B<658FA, @U 6
m65nFE7An :97@6, > 1300 - 4000
W@E;E7An ;6@8A?, >/7 500
"8>:8;6A9;F?S OB6:6PEF :;B>8F8FB=, U;6O. W ±60
GROUP 13 AMMUNITION
AND EXPLOSIVES
Class 1340 Rockets, Rocket Ammunition and Rocket Components
13 !", $" ! %
! $&"$" $ ' $
!5677 1340 89:;6<5=8>?8 ;6@8A?, BC DE8<E8 E7F6G8FB8 B 7E7A6<F?8 H67AB
S-8DM
This rocket is intended to engage various types of tar-
gets located in trenches, dugouts, earth and rock
embankments, defiles, terrain irregularities, caves and
similar shelters. The rocket warhead is filled with a fuel-
air explosive mixture.
Basic Characteristics
Caliber, mm 80
Length, mm 1,700
Weight, kg:
rocket 11.6
warhead 3.8
mixture 2.15
Firing range, m 1,300 - 4,000
TNT equivalent, kg 5.5 - 6
Rocket velocity, m/s 590
Operating temperature range,
o
C ±60
S-8T
This rocket is intended to engage modern tanks,
including those provided with explosive reactive armor,
lightly armored and soft-skinned combat materiel.
Owing to the fragmentation effect, the rocket also
inflicts damage upon manpower.
Basic Characteristics
Caliber, mm 80
Length, mm 1,680
Weight, kg:
rocket 15
warhead 6.6
explosive 1.6
Armor penetration, mm 400
Firing range, m 1,300 - 4,000
Rocket velocity, m/s 470
Operating temperature range, °C ±60
S-8DF
This rocket is intended to engage manpower and easi-
ly vulnerable materiel located in terrain irregularities
and open-type field fortifications.
Basic Characteristics
Caliber, mm 80
Length, mm 1,680
Weight, kg:
rocket 13.4
warhead 5.5
filler (mixture) 3.3
TNT equivalent, kg 6
Firing range, m 1,300 - 4,000
Rocket velocity, m/s 500
Operating temperature range,
o
C ±60
GROUP 13 AMMUNITION
AND EXPLOSIVES
Class 1340 Rockets, Rocket Ammunition and Rocket Components
13 !", $" ! %
! $&"$" $ ' $
!5677 1340 89:;6<5=8>?8 ;6@8A?, BC DE8<E8 E7F6G8FB8 B 7E7A6<F?8 H67AB
428
PART 2 2
UNGUIDED
AIRCRAFT ROCKETS
!"
-8-0
;8OF6PF6H8F6 O5= E7<8G8FB= >87AFE7AB < FEHFE8 <;8-
>=, =<5=8A7= ;6@8AES <7:E>EU6A85nFEUE F6PF6H8FB=.
=>?@>AB CDEDFGBEH=GHFH
!65BD;, >> 80
m5BF6, >> 1632
6776, @U:
;6@8A? 12,1
DE8<ES H67AB 4,3
7E7A6<6 1
WB56 7<8A6, @O 2 C 10
6
;8>= O8S7A<B= 7<8A6, 7 30
m65nFE7An :97@6, > 4000 - 4500
W@E;E7An ;6@8A?, >/7 545
"8>:8;6A9;F?S OB6:6PEF :;B>8F8FB=, U;6O. W ±60
-80
;8OF6PF6H8F6 O5= BFOB<BO965nFES P6GBA? 76>E58AE< B
<8;AE58AE< :9A8> :E7A6FE<@B < :8;8OF8S :E597a8;8 ED-
56@E< :;EAB<E;6OBE5E@6RBEFF?C EA;6Q6A858S (OB:E58S),
7EPO6TGBC :677B<F?8 :E>8CB ;6OBE5E@6RBEFF?> 7B7A8-
>6> F6<8O8FB= P8FBAF?C B 6<B6RBEFF?C @E>:58@7E< :8-
;8C<6A6 <EPO9oF?C R858S.
=>?@>AB CDEDFGBEH=GHFH
!65BD;, >> 80
m5BF6, >> 1632
6776, @U:
;6@8A? 12,3
DE8<ES H67AB 4,5
OB:E58S 2
m65nFE7An :97@6, > 2000 - 3000
W@E;E7An ;6@8A?, >/7 565
"8>:8;6A9;F?S OB6:6PEF :;B>8F8FB=, U;6O. W ±60
-810
;8OF6PF6H8F6 O5= >6;@B;E<6FB= < OF8<F?C 975E<B=C
F6P8>F?C R858S, >6;o;9AE< F6 >87AFE7AB, >87A <?76O@B
O876FAE<.
=>?@>AB CDEDFGBEH=GHFH
!65BD;, >> 80
m5BF6, >> 1605
6776, @U:
;6@8A? 11,1
DE8<ES H67AB 3,6
7F6;=Q8FB= 0,85
m65nFE7An :97@6, >:
O5= 76>E58A6 1800 - 3000
O5= <8;AE58A6 1300 - 2000
m65nFE7An <BOB>E7AB O?>6 F6 @EFA;67AFE> aEF8, @> 6
S-8-OM
This rocket is intended for terrain illumination at night.
It is an auxiliary purpose rocket.
Basic Characteristics
Caliber, mm 80
Length, mm 1,632
Weight, kg:
rocket 12.1
warhead 4.3
illuminating compound 1
Illumination intensity, cd 2 x 10
6
Illumination duration, s 30
Firing range, m 4,000 - 4,500
Rocket velocity, m/s 545
Operating temperature range,
o
C ±60
S-8PM
This rocket is intended to ensure individual protection
of aircraft and helicopters by setting up clouds of radar
reflective dipoles (chaffs) in the forward hemisphere
and thereby creating passive jamming to radar system-
s that control the air defense and air complexes to
intercept air targets.
Basic Characteristics
Caliber, mm 80
Length, mm 1,632
Weight, kg:
rocket 12.3
warhead 4.5
chaff 2
Firing range, m 2,000 - 3,000
Rocket velocity, m/s 565
Operating temperature range,
o
C ±60
S-8TsM
This rocket is intended to mark ground targets, routes
of movement and landing areas in daytime.
Basic Characteristics
Caliber, mm 80
Length, mm 1,605
Weight, kg:
rocket 11.1
warhead 3.6
filler 0.85
Firing range, m:
aircraft 1,800 - 3,000
helicopter 1,300 - 2,000
Smoke visibility range against contrast background, km 6
429
PART 2 2
UNGUIDED
AIRCRAFT ROCKETS
!"
GROUP 13 AMMUNITION
AND EXPLOSIVES
Class 1340 Rockets, Rocket Ammunition and Rocket Components
13 !", $" ! %
! $&"$" $ ' $
!5677 1340 89:;6<5=8>?8 ;6@8A?, BC DE8<E8 E7F6G8FB8 B 7E7A6<F?8 H67AB
S-13 UNGUIDED
AIRCRAFT ROCKETS
These rockets are intended to engage different kinds of
ground targets (from manpower to armor materiel and
hardened shelters) and can be used from the following
types of aircraft and helicopters: Su-24, Su-25, Su-27,
MiG-27, MiG-29, Mi-8, Mi-24, Mi-28, Ka-252 and
Ka-50.
Rockets are launched from B-13L and B-13L1 rocket
pods.
The S-13 unguided aircraft rockets are classified as air-
to-ground rockets. The basic rocket is a concrete-
piercing rocket, type S-13, comprising an extended
high-energy solid-propellant rocket motor and pene-
trating warhead.
The S-13 rocket boasts a number of modifications with
different warheads:
- S-13T with two-module HE fragmentation concrete-
piercing warhead;
- S-13-OF with HE fragmentation warhead;
- S-13D with fuel-air explosive warhead;
- S-13DF with enhanced power fuel-air explosive war-
head.
, $-. /" $!0!,," % "
! /" -13
;8_F6`F6H8F? _5= :E;6a8FB= F6`8>F?C b858c ;6`5BHFE-
dE <B_6 (EA aB<Ec 7B5? B D;EFB;E<6FFEc A8CFB@B _E E7EDE
:;EHF?C 9@;?ABc) B >Ed9A :;B>8F=Ae7= 7 76>E58AE< B <8;-
AE58AE<: f9-24, f9-25, f9-27, Bg-27, Bg-29, B-8,
B-24, B-28, !6-252, !6-50.
97@ ;6@8A E79G87A<5=8A7= B` D5E@6 E;9_Bc h-13
B h-131.
89:;6<5=8>?8 6<B6bBEFF?8 ;6@8A? () 7B7A8>? f-13
EAFE7=A7= @ ;6@8A6> @56776 «<E`_9C - `8>5=». h6`E<Ec ;6-
@8AEc 7B7A8>? =<5=8A7= D8AEFEDEcF6= F89:;6<5=8>6=
6<B6bBEFF6= ;6@8A6 f-13, 7E7AE=G6= B` <?7E@EkF8;d8-
ABHFEdE ;6@8AFEdE _<Bd6A85= A<8;_EdE AE:5B<6 DE5elEdE
9_5BF8FB= B :;EFB@6mG8c DE8<Ec H67AB.
6 D6`8 ;6@8A? f-13 7E`_6F b85?c ;=_ ED;6`bE< 7 ;6`-
5BHF?>B DE8<?>B H67A=>B (hn):
f-13" - 7 _<9C>E_95eFEc E7@E5EHFE-o9d67FEc D8AEFEDEc-
FEc hn;
f-13- p - 7 E7@E5EHFE-o9d67FEc hn;
f-13q - 7 EDr8>FE-_8AEFB;9mG8c 7>87em;
f-13qp - 7 EDr8>FE-_8AEFB;9mG8c 7>87em 97B58FFEc
>EGFE7AB.
S-13, S-13T
The S-13 is intended to destroy aircraft in reinforced
concrete shelters, as well as war materiel and man-
power in hardened shelters.
The S-13T is intended to destroy aircraft in different
types of shelters, including reinforced ones, demolish
runways and defeat command, control and communi-
cations posts and other objects.
The S-13T rocket is developed from the S-13 to
enhance its lethality owing to employment of two sep-
arable autonomous warheads: the first warhead is a
penetrating type (analog of the S-13 rocket warhead),
while the second one is a HE fragmentation warhead.
Design solutions, used to develop the S-13T rocket,
enabled the designers to increase the quantity of
explosives to be delivered behind a barrier and ensure
-13, -13
f-13 :;8_F6`F6H8F6 _5= 9FBHAEa8FB= 76>E58AE< < a858-
`ED8AEFF?C 9@;?AB=C, 6 A6@a8 EDr8@AE< <E8FFEc A8CFB@B
B aB<Ec 7B5? < E7EDE :;EHF?C 9@;?AB=C.
f-13" :;8_F6`F6H8F6 _5= 9FBHAEa8FB= 76>E58AE< < 9@;?-
AB=C ;6`5BHFEdE AB:6, < AE> HB758 B 97B58FF?C, @E>6F_-
F?C :9F@AE<, 6 A6@a8 <?<E_6 B` 7A;E= <`58AFE-:E76_EHF?C
:E5E7 6k;E_;E>E<, :9F@AE< 7<=`B B _;9dBC EDr8@AE<, 6
A6@a8 _5= 9FBHAEa8FB= @E>6F_F?C :9F@AE<.
f-13" ;6`;6DEA6F6 7 b85em :E<?l8FB= >Ed9G87A<6
f-13 `6 7H8A :;B>8F8FB= _<9C ;6`_85=mGBC7= 6<AE-
FE>F?C DE8<?C H67A8c, :8;<6= B` @EAE;?C =<5=8A7= :;E-
FB@6mG8c (6F65Ed hn f-13), <AE;6= - E7@E5EHFE-o9d67-
FEc. !EF7A;9@AB<F?8 ;8l8FB=, `65Ea8FF?8 :;B ;6`;6-
DEA@8 f-13", :E`<E5=mA F8 AE5e@E :E<?7BAe @E5BH8-
7A<E <`;?<H6AEdE <8G87A<6, `6FE7B>EdE `6 :;8d;6_9, FE B
430
PART 2 2
UNGUIDED
AIRCRAFT ROCKETS
!"
GROUP 13 AMMUNITION
AND EXPLOSIVES
Class 1340 Rockets, Rocket Ammunition and Rocket Components
13 !", $" ! %
! $&"$" $ ' $
!5677 1340 89:;6<5=8>?8 ;6@8A?, BC DE8<E8 E7F6G8FB8 B 7E7A6<F?8 H67AB
1234256 7898:;69<1;<:<
-13 -13
!65BD;, >> 122/90 122/90
q5BF6, >> 2540 3100
6776, @d:
;6@8A? 57 75
DE8<Ec H67AB 21 21+16,3
1,82 1,8+2,7
xoo8@AB<FE7Ae :;EDB<68A 3 > :;EDB<68A 6 >
d;9FA6 B 1 > d;9FA6 B 1 >
a858`ED8AEF6 a858`ED8AEF6
:5EG6_e ;6`;9l8FB= 20 >
2
q65eFE7Ae :97@6, > 1100 - 3000 1100 - 4000
f@E;E7Ae ;6@8A?, >/7 650 500
"8>:8;6A9;F?c _B6:6`EF
:;B>8F8FB=, d;6_. f ±60 ±60
Basic Characteristics
S-13 S-13T
Caliber, mm 122/90 122/90
Length, mm 2,540 3,100
Weight, kg:
rocket 57 75
warhead 21 21+16.3
explosive 1.82 1.8+2.7
Effectiveness penetrates 3 m penetrates 6 m
of earth and 1 m of earth and 1 m
of reinforced of reinforced
concrete concrete
runway demolition area, 20 m
2
Firing range, m 1,100 - 3,000 1,100 - 4,000
Rocket velocity, m/s 650 500
Operating temperature range,
o
C ±60 ±60
the optimal spread of warhead blasting zones behind
the barrier that made it possible to sharply increase the
effectiveness of the S-13T rocket compared with the
S-13, maintaining its penetration capability.
The S-13T rocket development is based on the modu-
lar principle, providing for the exclusion of the second
warhead (second module) (in this case the S-13T turn-
s into the S-13) or its replacement with another pur-
pose warhead.
ED87:8HBAe ;6`F878FB8 `EF :E_;?<6 DE8<?C H67A8c `6
:;8d;6_Ec, HAE ;8`@E :E<?l68A koo8@AB<FE7Ae :E
7;6<F8FBm 7 f-13 :;B 7EC;6F8FBB :;EFB@6mG8c 7:E-
7EDFE7AB.
E7FE<9 ;6`;6DEA@B f-13" :E5Ea8F :;BFbB: >E-
_95eFE7AB, :E`<E5=mGBc <AE;9m DE8<9m H67Ae (<AE;Ec
>E_95e) 5BDE B7@5mHBAe (< kAE> 759H68 f-13" :;8-
<;6G68A7= < f-13), 5BDE `6>8FBAe F6 DE8<9m H67Ae _;9dE-
dE F6`F6H8FB=.
-13
S-13
-13T
S-13T
431
PART 2 2
UNGUIDED
AIRCRAFT ROCKETS
!"
S-13-OF, S-13D, S-13DF
These rockets are intended to engage lightly armored,
easily vulnerable materiel and manpower.
The S-13-OF is a rocket
with a HE fragmentation
warhead with pre-
formed diamond-
shaped splinters.
The warhead is
equipped with a tail
fuze. To delay the fuze
operation time, the
warhead is fitted with
an elongated noze cap.
The S-13D is a rocket
whose warhead is filled
with fuel-air single-
action explosive mixture
and fitted with a point
contact fuze.
The S-13DF is a rocket
with an enhanced power
warhead filled with fuel-
air explosive mixture.
Unguided aircraft rock-
ets are classified
according to use as
main and auxiliary (spe-
cial).
-13-F, -13G, -13GF
;8_F6`F6H8F? _5= :E;6a8FB= 58d@ED;EFB;E<6FFEc, 58d-
@E9=`<B>Ec A8CFB@B B aB<Ec 7B5?.
f-13- p - ;6@8A6 7 E7@E-
5EHFE-o9d67FEc DE8<Ec
H67Aem 7 `6_6FF?> _;ED-
58FB8> F6 E7@E5@B ;E>-
DE<B_FEc oE;>?. hn
9@E>:58@AE<6F6 <`;?<6-
A85eF?> 97A;Ec7A<E>
_EFFEdE AB:6. q5= @E>:8-
F76bBB `6d59D58FB= hn <
d;9FA `6 <;8>= `6_8;a@B
< 7;6D6A?<6FBB <`;?<6-
A85eFEdE 97A;Ec7A<6 ()
< @EF7A;9@bBB :;B>8F8FE
:;E7AE8 B F6_8aFE8 ;8-
l8FB8: dE5E<FEc 9_5B-
F8FF?c F6@EF8HFB@.
f-13q - ;6@8A6 7 DE8<Ec
H67Aem, 7F6;=a8FFEc
EDr8>FE-_8AEFB;9mG8c
7>87em E_FE6@AFEdE _8c-
7A<B=. hn 9@E>:58@AE<6F6
dE5E<F?> @EFA6@AF?> <`-
;?<6A85eF?> 97A;Ec7A-
<E>.
f-13qp - ;6@8A6 7 hn :E-
<?l8FFEdE >Ed9G87A<6,
7F6;=a8FFEc EDr8>FE-
_8AEFB;9mG8c 7>87em.
89:;6<5=8>?8 6<B6bB-
EFF?8 ;6@8A? () < `6-
<B7B>E7AB EA ;8l68>?C
`6_6H :E_;6`_85=mA7= F6
;6@8A? E7FE<FEdE B <7:E-
>Ed6A85eFEdE (7:8bB65e-
FEdE) F6`F6H8FB=.
GROUP 13 AMMUNITION
AND EXPLOSIVES
Class 1340 Rockets, Rocket Ammunition and Rocket Components
13 !", $" ! %
! $&"$" $ ' $
!5677 1340 89:;6<5=8>?8 ;6@8A?, BC DE8<E8 E7F6G8FB8 B 7E7A6<F?8 H67AB
1234256 7898:;69<1;<:<
-13-F -13G -13GF
!65BD;, >> 122 122 120(hn)/122
q5BF6, >> 2898 3120 3120
6776, @d:
;6@8A? 69 68 68
DE8<Ec H67AB 33 32 32
7 - -
7>87B - 14,6 14,6
xoo8@AB<FE7Ae 450 E7@E5@E< A;EAB5E<?c A;EAB5E<?c
:E 25 - 35 d k@<B<658FA k@<B<658FA
35 - 40 @d _E 40 @d
q65eFE7Ae :97@6, > 1600 - 3000 1600 - 3000 500 - 6000
fED7A<8FF6= 7@E;E7Ae, >/7 530 530 530
"8>:8;6A9;F?c _B6:6`EF
:;B>8F8FB=, d;6_. f ±60 ±60 ±60
Basic Characteristics
S-13-OF S-13D S-13DF
Caliber, mm 122 122
120(Whd)/122
Length, mm 2,898 3,120 3,120
Weight, kg:
rocket 69 68 68
warhead 33 32 32
explosive 7 - -
mixture - 14.6 14.6
Effectiveness 450 fragments, TNT TNT
25 - 35 g each equivalent equivalent
35 - 40 kg up to 40 kg
Firing range, m
1,600 - 3,000 1,600 - 3,000 500 - 6,000
Rocket velocity, m/s 530 530 530
Operating temperature
range,
o
C ±60 ±60 ±60
-13G
S-13D
-13GF
S-13DF
-13-F
S-13-F