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GROUP 15 AIRCRAFT AND AIRFRAME

STRUCTURAL COMPONENTS

Class 1550 Drones

 15  

 ! " #  $ %! !"

 1550     

678

PART 4 #  4

TRAINING TARGETS )*+,-*

TRAINING TARGET-RICH ENVIRONMENT

Intended for quality practice in combat readiness mis-

sions of air defense assets and features different type-

s and number of targets simultaneously flying from dif-

ferent directions at various altitudes and speeds.

The 9F841 Saman target missile is derived from the

9M33M2 SAM of the Osa-AK system and can be used

to simulate the strike of Shrike antiradar missiles.

The RM-5V27A Pishchal and RM-5V27M target missiles

are developed from the 5V27 SAM of the S-125

system. In terms of configuration and speed character-

istics, they are similar to such air attack weapons as the

SRAM, Tomahawk, HARM, Martel, Tacit-Rainbow, and

others.

The most economical method of creating a training

target-rich environment is launching from an

autonomous post based on the 5P73 mobile launcher

of the S-125M1 air defense system. The RM-5V27

target missiles are loaded on the launcher in a con-

ventional mode, while the 9F841D missiles are loaded

via a special adapter attached to the 5P73 launcher.

Each 5P73 launcher can mount up to four target

missiles. To provide the launcher drives with power

and to spin the missile gyroscopes, use is made of

the standard 5E96A diesel power plant (30 kW). The

preparation and launch are effected by a special sys-

tem (control panel) without involving the automatic

*!!+", *-, !. !"%

OPQR PS RTU V QPR VTU

WT PT OXY  ZQ[S Q -

  RT \U, PT ZPS]ZS T

TQP[Z  QZ TZ, S]Z  QZ T-

U  Q S.

- VQ ^_` 9)^^)2  «Y-b» QP -

-d 9e841 («f»), S g V -

QT PS \ [P T\Z 

«+U».

- VQ ^_` 5X27  f-125 QP --

d `)-5X27b («O]»)  `)-5X27),   W-

 [   Z VQ 

 fX-,  f`h), iZ, j, ), ik-

`UV[  P.

-V kRU V QPS W\TU

VT - [  TW dW 

(b)-)  VQ PTgU [TU [T (O_)

5O73  f-125)1. O k QW[Q `)-5X27 

O_ - dS,  dU 9e841l - RQ \U

P (ZP), U QSS  O_ 5O73.

- gP[m O_ 5O73 g [T P RZ d-

U. lS S kkWU TPT O_  -

[ WT dU  PWT Z  [[ -

Q[S dS PQ-Q\S (lhf) 5,96b

(30 X). OPWT  Q[ QTPSS \U

U ([) VQ [RS TU T

GROUP 15 AIRCRAFT AND AIRFRAME

STRUCTURAL COMPONENTS

Class 1550 Drones

 15  

 ! " #  $ %! !"

 1550     

679

PART 4 #  4

TRAINING TARGETS )*+,-*

Basic Characteristics

Training target 9F841A RM-5V27A

Range, km 18 - 25 up to 30 40 - 50 70 - 85

Altitude, km up to 13 3.5 15 50

Flight time, s up to 100 75 125 200

ERA, m

up to 1.3 up to 0.3

Speed, m/s 350 - 150 500 - 150

Trajectory toss ballistic ballistic ballistic

launching equipment of the S-125M1 system. The

time of launch preparation does not exceed 30 s. The

missiles are controlled autonomously from the

onboard programmer without using the missile guid-

ance station. This provides for an unlimited number of

in-flight targets, which is the basis for creating a

training target-rich environment. To launch target

missiles, the skill of the air defense system combat

crew is quite sufficient, and no additional special

training is required. The possibility of transporting the

5P73 launchers and the 5E96-A diesel power plant

ensures a training target-rich environment at any

range for any air defense system. The expenditures

to reequip 5V27 and 9M33M2 SAMs are insignifican-

t, hence, the cost of targets is low.

A mass air attack can be simulated by kinematic para-

meters (direction, altitude, range) as well as by radar

signature (ERA of various type targets) and target fly-

by frequency. As an option, launches can be made first

by Saman-A target missiles, in the direction of a firing

air defense system with a minimal parameter

(simulation of the Shrike missile attack), then by RM-

5V27A target missiles (simulation of cruise missile

flight). The employment of several autonomous training

target posts makes it possible to simulate a multiple

wave air strike for the air defense assets under check.

The important feature of training targets is their low

cost and ease of operation.

The proposed version of creating the training target-

rich environment is the most economical, while suc-

cessful firing in these conditions guarantees the

repulse of any mass air raid.

 fY125)1. XS PWT  [[ -  V-

 30 [P. fV [TS  TU, 

VTW WW [UT,  V[m]U -

\ TPS . h QTS  WRT -

RT ZPS]ZS T  dU, R  STSS

TU PS QPS W\TU dU VT-

. lS Z [T Tq\ VTW R ^` P-

R  P \W V[RS  -

V[S. XQg TS [TZ [-

T 5O73  lhf 5,96-b QTS WQT W-

\T[m d[m VT[  mVZ PSZ 

PS mVZ ^`. ) Q  V[P-

T ^_` 5X27  9)^^)2 QR, PT-

,  dU TS.

)T TQP[d P g -

TS   R  (T,

T, P),    P\U Q-

 ( hO` dU QZ T)  TU -

 PTS dU.  T W[ V P-

g [, T T[m RP, dU «f-b» T

T  Sm]U ^`   -

 (\S  «+U»),  Q [ d-

U `)-5X27b (\S  Z ). *-

QT Z TZ dZ T

QT PT WkdTU TQ-

P[dU [P PS TSZ PT OXY. Xg q-

 S dU STSS Z PdTQ 

 k[\.

OPWU T QPS W\TU d-

U VT STSS V kR,  [-

dS V T kZ [TSZ W[ g

mVW TW TQP[dW .

!<=>?=@A BCDCEFADG<FGEG

)d 9H841 *-5"27

l,  18 - 25 P 30 40 - 50 70 - 85

X,  P 13 3,5 15 50

XS,   P 100 75 125 200

hO`, 

P 1,3 P 0,3

f, / 350 - 150 500 - 150

i V V V

 VT

GROUP 15 AIRCRAFT AND AIRFRAME

STRUCTURAL COMPONENTS

Class 1550 Drones

 15  

 ! " #  $ %! !"

 1550     

680

PART 4 #  4

TRAINING TARGETS ()*+,)

!'()*(+, -./.01,/2'1202

-,  250

0,  5,72

(, 2 330

4 56 ,  46

0 8 59,  100

49 - 5:29,  4,5 - 9

(9  =, /:

: @ :2 A8 1300

 : 20 

 B59C A8  830

D 59 =

 8E 8, :

 5 ±9

: -: : ±6,5

G :9 , . 3,2

IAE 5J 9, 25. K ±40

Basic Characteristics

Caliber, mm 250

Length, m 5.72

Weight, kg 330

Missile climb altitude, km 46

Range to fall point, km 100

Motor operation time, s 4.5 - 9

Maximum speed of training target, m/s:

at end of active flight leg 1,300

at 20 km altitude

at trajectory's descending leg 830

Fall zone measured

from estimated point, km:

in range ±9

in deflection ±6.5

Total time of flight, min 3.2

Operating temperature range,

C±40

96M6M BALLISTIC

TRAINING TARGET

Intended to train flying personnel of the air defense air

arm and assess the combat effectiveness of ballistic

missiles interception systems.

The 96M6M is essentially an unguided missile simulat-

ing, by the values of its effective reflective area (ERA)

and speed at the descending leg of the ballistic trajec-

tory, a real high-speed missile.

The training target comprises a nose fairing, instrument

section and solid-propellant motor. The instrument

section accommodates a transceiver to help determine

current coordinates of the training target with the aid of

the Kama radar systems, which provides for assess-

ment of the trajectory parameters.

The training targets are launched by a two-tube

ground-based launcher, type 89Ts6-02.

The training target is detected and tracked by an AD

missile system, which receives a signal returned from

the training target.

The 96M6M is complete with test equipment for

prelaunch checkouts and launch of training targets.

> # %?

@A 96@6@

G5J8 59 -A89 2 : :E G4h

 @ -:E ijj:  B: --

8B .

(= 96(6( - A:99 , AkC9 

:8 ijj:E lkCE :B (mGn) 

  B59C A8 -8E -

 :Ak A.

(=  J 2:2 -9, -2 -

  5:29  :5 :. 4 - -

 A: 58 59 59 A-

CB 5     C J-

B : noK «», 8 J:9 @ -

 .

DA =E J:59  5:AB:E JE

A:E A: 89r6-02.

h-Al  :l5 = J:59

5:  DnK  lA  :B-

 = 2A.

96(6( A9 -:8E -

AE, J:9kCE :5 5: :

 JA =E.

GROUP 15 AIRCRAFT AND AIRFRAME

STRUCTURAL COMPONENTS

Class 1550 Drones

 15  

 ! " #  $ %! !"

 1550     

681

PART 4 #  4

TRAINING TARGETS ()*+,)

9F841 SAMAN TARGET MISSILE

Intended to simulate current and prospective air target-

s during the training of crews of air defense missile

systems used at regimental, divisional and army levels

in air defense, air force and naval units, as well as dur-

ing operational development and trials of new AD mis-

sile systems.

The 9F841 Saman is a small-size solid-propellant mis-

sile used as an air target simulator (ATS). It was devel-

oped from the basic 9FM33M2 (M3) AD missile. In

terms of its geometric, ballistic and radar characteris-

tics, it is similar to such air attack weapons as the

BGM-34 drone, ALCM and HARM cruise and antiradar

missiles and Walleye guided air bombs.

The Saman is a single-stage missile of the canard con-

figuration with a freely rotating tail. It is launched in a

tilted position and controlled in flight until it reaches

the desired altitude from an autonomous 9A33AM2

combat vehicle of the Osa-AK AD missile system (un-

modified).

The 9F841 ATS, the combat vehicle and standard set of

the Osa-AK AD missile system make up a 9F691 train-

ing target set. Once it has reached the desired altitude,

the ATS may fly independently or make a 5-second

pitchup maneuver at the 28th or 40th second of flight

or can fly without maneuvering. The combat vehicle

allows for the control of two missiles launched at a

5-second interval. In flight, the ATS can be detected

and tracked in the radar and IR frequency bands and

also observed visually.

%-*+ 9,841 « *»

OPQR PS T UV  U-

V UQPWXV TY  ZWR ZUV RU Q-

-V U ([\) U], PUQ-

]  Y] QUU U UYV O^_, ^^`  ^(a, 

b PS Z  Y QPUV Q-

V .

(QS UPUS  9a841 «`» -

 UQPWXV TY ()^e) - QZ  ZQ

QY WUSY  9a(33(2 ((3). O U

]R, ZR  PT V-

  ZQ   PU UQPWX]

PS,  ZY Y  BGM-34,

  UPT   AL`(,

«f», WUS UT ZZ «gY».

[W  WU  P R UUP  ZW-

Wh UW QUPS  UY PUbY Z-

UY X (() 9i33i(2 Q] ] -

 ([\) «_-i» (QWS ZQ PZ),  -

Y.

)^e 9a841, ZUS X  XY  Q-

] ZWPUS [\ «_-i» USh XY

 9a691. O UVP  ZWWh UW -

 )^e b WjUSS U   U-

 «ZU» U R 5   28   40  Z

ZQ U. US X QUS WUS PUWS

, QWj  U 5 . ^ T -

 ZRUS UQb ZWbS  -

UbPS )^e U PT  k P-

QV R,  b ] UQW] ZhPS.

GROUP 15 AIRCRAFT AND AIRFRAME

STRUCTURAL COMPONENTS

Class 1550 Drones

 15  

 ! " #  $ %! !"

 1550     

682

PART 4 #  4

TRAINING TARGETS ()*+,)

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l ,  P 22

lQ U ,  0,05 - 5

`  U Q S, / 150 - 250

(S P ,  120

` WUS PPS

 US  ]

nO\  R 15 ooT, 

0,6

` PS, ]P. ±3

oZ Q, :

P 3,16

P 0,21

QV  0,65

(XY  9a691

RU )^e  ( 6

l, :

PWUS]  13,5

UQbY UPT )^e 11

^S ]U  ZUW h, . 1

Basic Characteristics

Launch weight, kg 123.5

Flight range, km up to 22

Flight altitude envelope, km 0.05 - 5

Flight speed in employment zone, m/s 150 - 250

Maximum flight duration, s 120

Control radio command or

autonomous by a program

ERA at 15 GHz frequency, m

0.6

Fall sector, deg ±3

Overall dimensions, m:

length 3.16

diameter 0.21

wing span 0.65

Training target set 9F691

Number of ATS per combat vehicle 6

Range, km:

flight with radio control 13.5

possible self-destruction of ATS 11

Warmup time, min 1

GROUP 15 AIRCRAFT AND AIRFRAME

STRUCTURAL COMPONENTS

Class 1550 Drones

 15  

 ! " #  $ %! !"

 1550     

683

PART 4 #  4

TRAINING TARGETS )*+,-*

RM-5V27 PISHCHAL TARGET MISSILE

Intended to simulate current and prospective air target-

s during the training of crews of air defense missile-gun

and missile systems used by air defense units, as well

as during operational development and trials of new AD

missile systems and radars.

The RM-5V27 Pishchal is a solid-propellant target

missile. It was developed from the basic 5V27(D) AD

guided missile. In terms of its geometric, ballistic and

radar characteristics, it simulates small-size air attack

weapons.

The Pishchal is a two-stage (sustainer and booster)

missile of the canard configuration. For launch and

control, it uses the unmodified series-produced 5P73

(5P71) launcher and the control station of the

S-125(M) AD missile system. At the initial leg of the

RM-5V27 missile injection into its trajectory, it is con-

trolled in a standard way, by radio commands from the

SNR-125 guidance radar. Then

the airborne programmer takes

over. The flight trajectory may be

level or include nose-up or nose-

down (at an angle of 5 to 70

)

pitching maneuvers (with an

acceleration of 2 to 8 g). Two

training targets may be launched

at a 5-second interval. In flight,

the target missile can be detect-

ed and tracked in a radar fre-

quency band and observed visu-

ally due to its motor exhaust

flame and, after the motor ceas-

es to function, by the flare flame.

Its launching safety is enhanced

by the availability of the self-

destruction system. In service,

the target missile is maintained

with the use of the standard set

of ground equipment of the S-

125(M) AD missile system. The

training target set can function at

an ambient temperature of -40 to

+50

%-,- ,-5"27 «/»

NOPQ OR S TU  T-

U TPOVWU SX  YVQ YTU QT P-

U -VWQU (Z[N)  P-U

(Z[) T T TXU N\],  ^ OR Y 

X POTU P-U   [_`.

aTOTR -W [)-5\27 «Nc» P-

Y  YP PX VTRX  5\27(e).

N T fQ, YQ  O-

S U  V P

OT TPOVWf OR.

[ «Nc» OTVUVQR ( P WTX

V  VR), T  gOQX

U «V». eR PV  VTR PVhR YP

OY XR VTR VT 5N73 (5N71) 

SR VTR Z[ `-125 ()). iT  Q-

 VQ TTO [)-5\27  h PTO-

R T W ^ S TOR `-[-125  -

OO  UO  T-

 VT  -

f-Of VXT

. aR  ^

Y  YP T,    -

T «YT» ( -

fVPX 2-8 g)  «T»

(O Vf 5-70°). \P^ P-

V OTVU WX  T

5 . \ S  

YQTR TP^ 

YV^R  T^OR T

OS OP Q-

,  ^ TPVf Yh-

OR  kV OTfR,  -

 QR f Y - 

kV . P

VT TWR P Q -

 TOS. N gV-

S PVR WX

 Pf YVOT-

R Z[ `-125 ()). )WX

 ^ kVS-

T  V V^h-

cX O  -40 O +50° `.

Basic Characteristics

Weight, kg:

sustainer stage 939.2

booster 407.5

Flight altitude envelope, km 0.1 - 6

Firing zone, km 12 - 30

Time, s:

motor operation 22

possible destruction up to 20

Control radio commands and

autonomous by a program

Accuracy of desired course attainment, deg ±5

Overall dimensions, m:

length (with booster) 5.948

length of sustainer stage 4.134

diameter of sustainer stage 0.375

Number of missiles placed on launcher 4 (2)

!:;<=;>? @ABACD?BE:DECE

), f:

WTX V 939,2

VR 407,5

eP T ,  0,1 - 6

Z Y,  12 - 30

\R, :

Y OTfR 22

TP^X TOS  TTO O 20

` VTR OOR

 TR  f

aQ TTO  VV, fO. ±5

qY P, :

O ( V) 5,948

O WTX V 4,134

O WTX V 0,375

QT   Ni 4 (2)

687

PART 5  5

ROUNDS FOR TANK

AND ANTITANK GUNS

 

   

GROUP 13 AMMUNITION AND EXPLOSIVES

Class 1315 Ammunition

of 75 to 125 mm

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

0122 1315 3456786129 8 17:800578;2<85 =92:7509

<108>71 4: 75 ?? @4 125 ?? =<0AB8:50CD4

125mm 3VBM17 ROUND WITH 3BM42

APFSDS PROJECTILE FOR D-81 GUN

The round is intended to engage modern updated

tanks provided with combined armor protection.

125-44 $" 5 3$617  7 87"6

9%5! 7"6 7:96 3642 % ;% 9-81

75@D1QD1B5D @0R 2:750C>9 64 24=75?5DD9? ?4@57D8Q8-

74=1DD9? :1D<1?, 8?5AU8? <4?>8D874=1DDVA >74D5Q1-

U8:V.

125mm TANK ROUND

WITH APFSDS PROJECTILE

The rounds is intended for firing from the D-81 gun

against current modernized and future tanks with

sophisticated composite armor with add-on ERA plates.

Basic Characteristics

Weight, kg:

round 20.3

projectile with increment propelling charge 10.7

Muzzle velocity, m/s 1,750

Operating temperature range,

C from -40 to +50

125-44 7%$"8 $" 5

 7 87"6 9%5! 7"6 7:96

75@D1QD1B5D @0R 2:750C>9 8Q :1D<4=4; 6Vb<8

c-81 64 24=75?5DD9? ?4@57D8Q874=1DD9? 8 657-

265<:8=D9? :1D<1?, 42D1U5DD9? 204dD4; <4?64Q8-

e84DD4; >74D5;, V2805DD4; @8D1?8B52<4; Q1U8:4;.

EFGHFIJ KLMLNOJMPEOPNP

f1221, <g:

=92:7501 20,3

2D17R@1 2 @4640D8:50CD9? Q17R@4? 10,7

1B10CD1R 2<4742:C, ?/2 1750

c8161Q4D h<260V1:1e84DD9i :5?6571:V7, g71@.  4: -40 @4 +50

Basic Characteristics

Weight, kg:

round 20.4

projectile 7.05

Muzzle velocity, m/s 1,700

Operating temperature range,

C from -40 to +50

EFGHFIJ KLMLNOJMPEOPNP

f1221, <g:

=92:7501 20,4

2D17R@1 7,05

1B10CD1R 2<4742:C, ?/2 1700

c8161Q4D h<260V1:1e84DD9i :5?6571:V7, g71@.  4: -40 @4 +50

3B3M17

3VBM17

92:750 2 3

Round with APFSDS projectile

688

PART 5  5

ROUNDS FOR TANK

AND ANTITANK GUNS

 

  

GROUP 13 AMMUNITION AND EXPLOSIVES

Class 1315 Ammunition

of 75 to 125 mm

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

0122 1315 3456786129 8 17:800578;2<85 =92:7509

<108>71 4: 75 ?? @4 125 ?? =<0AB8:50CD4

125mm 3VBK16 ROUND WITH 3BK18M

HEAT PROJECTILE FOR D-81 GUN

The round is intended for use against armored targets,

manpower, fortifications, engineer constructions, fire

positions of artillery pieces, mortars and launchers.

125-44 $" 5 3$%16  %657!$8"6

8796 3%186 % :% 9-81

75@D1PD1B5D @0Q 2:750C>9 64 >74D874=1DD9? R50Q?, 1

:1<S5 S8=4; 2805, T47:8T8<1R84DD9? 8 8DS5D57D9? 24-

47VS5D8Q?, 4WD5=9? 64P8R8Q? 17:8005788, ?8D4?5:4=,

71<5:D9X V2:1D4=4<.

;<=><?@ ABCBDE@CF;EFDF

Y1221, <W:

=92:7501 29,0

2D17Q@1 19,0

1B10CD1Q 2<4742:C, ?/2 905

^8161P4D _<260V1:1R84DD9X :5?6571:V7, W71@.  4: -40 @4 +50

Basic Characteristics

Weight, kg:

round 29.0

projectile 19.0

Muzzle velocity, m/s 905

Operating temperature range,

C from -40 to +50

125mm 3VBK25 ROUND WITH 3BK29M

HEAT PROJECTILE FOR D-81 GUN

The round is intended for use against hard armored

targets, including those provided with explosive reac-

tive armor and concealed behind masks, as well as

manpower, fortifications, engineer constructions, fire

positions of artillery pieces, mortars and launchers.

The projectile’s specific feature is a filler pressed into

the body.

125-44 $" 5 3$%25  %657!$8"6

8796 3%296 % :% 9-81

75@D1PD1B5D @0Q 2:750C>9 64 ?4kD9? >74D874=1DD9?

R50Q?, = :4? B8205 42D1k5DD9? D1=52D4; @8D1?8B52<4;

P1k8:4; 8 V<79:9? P1 ?12<874=4BD9?8 275@2:=1?8, 1

:1<S5 64 S8=4; 2805, T47:8T8<1R84DD9? 8 8DS5D57D9?

2447VS5D8Q?, 4WD5=9? 64P8R8Q? 17:8005788, ?8D4?5:4=,

71<5:D9X V2:1D4=4<.

:08B8:50CD1Q 424>5DD42:C 2D17Q@1 - 2D17QS5D85 6752-

24=1D85? = <476V2.

;<=><?@ ABCBDE@CF;EFDF

Y1221, <W:

=92:7501 28,4

2D17Q@1 18,4

1B10CD1Q 2<4742:C, ?/2 915

^8161P4D _<260V1:1R84DD9X :5?6571:V7, W71@.  4: -40 @4 +50

Basic Characteristics

Weight, kg:

round 28.4

projectile 18.4

Muzzle velocity, m/s 915

Operating temperature range,

C from -40 to +50

33K16

3VBK16

33K25

3VBK25

689

PART 5  5

ROUNDS FOR TANK

AND ANTITANK GUNS

 

   

GROUP 13 AMMUNITION AND EXPLOSIVES

Class 1315 Ammunition

of 75 to 125 mm

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

1233 1315 456789723: 9 28;911689<3=96 >:3;861:

=219?82 5; 75 @@ A5 125 @@ >=1BC9;61DE5

125mm 3VP6 ROUND WITH 3P31 PRACTICE

APFSDS PROJECTILE FOR D-81 GUN

The round is intended for practice firings to develop

practical skills in accurate firing.

125-22 $" 3 3$6  %! %!4

5%3! 6"4 6754 331 % 8% 5-81

86AE2PE2C6E A1Q RC6?E5-?56>:T 3;861D?, 789 =5;58:T

7895?86;2B;3Q 782=;9C63=96 E2>:=9 > ;5CE53;9 3;861D?:.

Basic Characteristics

Weight, kg:

round 19.5

projectile 5.2

Muzzle velocity, m/s 1,830

Operating temperature range,

C from -40 to +50

BCDECFG HIJIKLGJMBLMKM

`2332, =a:

>:3;8612 19,5

3E28QA2 5,2

2C21DE2Q 3=5853;D, @/3 1830

b9272P5E c=371R2;2d95EE:T ;6@7682;R8, a82A.  5; -40 A5 +50

125mm 3VOF36 ROUND WITH 3OF26

HE FRAGMENTATION PROJECTILE FOR D-81 GUN

The round is intended for use against manpower, field

fortifications, engineer constructions, fire positions of

artillery pieces, mortars, launchers and infantry fire

weapons.

The projectile’s specific feature is a portion pressed

filler.

125-22 $" 3 3$N36  %36-

N6"4 6754 3N26 % 8% 5-81

86AE2PE2C6E A1Q 3;861D?: 75 g9>5< 3916, 7516>:@

R=86716E9Q@, 9Eg6E68E:@ 3558Rg6E9Q@, 5aE6>:@ 75P9-

d9Q@ 28;9116899, @9E5@6;5>, 862=;9>E:T R3;2E5>5=, 76-

T5;E:@ 5aE6>:@ 386A3;>2@.

;19C9;61DE2Q 535?6EE53;D 3E28QA2 - 3E28Qg6E96 758d9-

5EE:@ 786335>2E96@.

BCDECFG HIJIKLGJMBLMKM

`2332, =a:

>:3;8612 33,0

3E28QA2 23,0

2C21DE2Q 3=5853;D, @/3 850

b9272P5E c=371R2;2d95EE:T ;6@7682;R8, a82A.  5; -40 A5 +50

Basic Characteristics

Weight, kg:

round 33.0

projectile 23.0

Muzzle velocity, m/s 850

Operating temperature range,

C from -40 to +50

3h36

3VOF36

36

3VP6

690

PART 5  5

ROUNDS FOR TANK

AND ANTITANK GUNS

 

   

GROUP 13 AMMUNITION AND EXPLOSIVES

Class 1315 Ammunition

of 75 to 125 mm

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

1233 1315 456789723: 9 28;911689<3=96 >:3;861:

=219?82 5; 75 @@ A5 125 @@ >=1BC9;61DE5

125mm 3VP5 ROUND WITH 3P11 PRACTICE

HEAT PROJECTILE FOR D-81 GUN

The round is intended for practice firings to develop

practical skills in accurate firing when there is no need

for the destructive and casualty effect of the projectile

on the target.

125-11 $" 2 3$5  %! %!3

%324!$5"3 5463 311 % 7% 6-81

86AE2SE2C6E A1T UC6?E5-?56>:W 3;861D?, 789 785>6A6-

E99 =5;58:W 7895?86;2B;3T 782=;9C63=96 E2>:=9 > ;5C-

E53;9 3;861D?: 9 E6; E65?W5A9@53;9 > 82S8UY2BZ6@ 9

7582[2BZ6@ A6<3;>99 3E28TA2 U \619.

89:;9<= >?@?AB=@C8BCAC

]2332, =^:

>:3;8612 29,0

3E28TA2 19,0

2C21DE2T 3=5853;D, @/3 905

a9272S5E b=371U2;2\95EE:W ;6@7682;U8, ^82A.  5; -40 A5 +50

Basic Characteristics

Weight, kg:

round 29.0

projectile 19.0

Muzzle velocity, m/s 905

Operating temperature range,

C from -40 to +50

125mm 3VBK25IN ROUND

WITH 3BK29IN PRACTICE

HEAT PROJECTILE FOR D-81 GUN

The round is intended for practice firings to develop

practical skills in accurate firing when there is no need

for the destructive and casualty effect of the projectile

on the target.

125-11 $" 2 3$%25!5  %! %!3

%324!$5"3 5463 3%29!5

% 7% 6-81

86AE2SE2C6E A1T UC6?E5-?56>:W 3;861D?, 789 785>6A6-

E99 =5;58:W 7895?86;2B;3T 782=;9C63=96 E2>:=9 > ;5C-

E53;9 3;861D?: 9 E6; E65?W5A9@53;9 > 82S8UY2BZ6@ 9

7582[2BZ6@ A6<3;>99 3E28TA2 U \619.

Basic Characteristics

Weight, kg:

round 28.4

projectile 18.4

Muzzle velocity, m/s 915

Operating temperature range,

C from -40 to +50

89:;9<= >?@?AB=@C8BCAC

]2332, =^:

>:3;8612 28,4

3E28TA2 18,4

2C21DE2T 3=5853;D, @/3 915

a9272S5E b=371U2;2\95EE:W ;6@7682;U8, ^82A.  5; -40 A5 +50

35

3VP5

3425

3VBK25IN