Каталог - Оружие России 2000 c82-795

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668

PART 4  4

AUTOMATED CONTROL SYSTEMS

AND FACILITIES

 

  !"#

GROUP 12 FIRE CONTROL EQUIPMENT

Class 1210 Fire Control Systems,

Complete

 12   !"# $%&'" " $("' ($!')

45677 1210 89:;69<=<>:86??@A 7<79A;@

BC>685A?<D 8:E7F6;<

Krym-S1E Automation System

for Use of Airspace Planning

by Area ATC Center

Serves for the automation of collection of ATC flight-

plan information, planning the use of airspace by area

ATC centers and the transmission of this information to

cooperating AD command posts and ATC centers.

Basic Characteristics

Number of simultaneously:

stored standard aircraft flight plans

(scheduled flights) up to 10,000

processed flight requests

for current day up to 3,000

indicated flight tracks under flight plans up to 100

interfaced information

sources (airfields) up to 16

interfaced cooperating control elements up to 9

Operation mode continuous, 24 h

Design version stationary

Krym-S2E Automation System for

Use of Airspace Planning by

Zone ATC Center

Serves for the automation of collection of ATC flight-

plan information, planning the use of airspace by zone

ATC centers and the transmission of this information to

cooperating AD command posts and ATC centers.

Basic Characteristics

Number of simultaneously:

stored standard aircraft flight plans

(scheduled flights) up to 20,000

processed flight requests

for current day up to 6,000

indicated flight tracks under flight plans up to 100

interfaced information

sources

(airfields, ATC centers) up to 14

interfaced cooperating control elements up to 14

Operation mode continuous, 24 h

Design version stationary

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669

PART 4  4

AUTOMATED CONTROL SYSTEMS

AND FACILITIES

 

  !"#

GROUP 12 FIRE CONTROL EQUIPMENT

Class 1210 Fire Control Systems,

Complete

 12   !"# $%&'" " $("' ($!')

45677 1210 89:;69<=<>:86??@A 7<79A;@

BC>685A?<D 8:E7F6;<

Krym-KTE Airspace Control

Automation System for

AD Elint Formation (Unit)

Designed to automatically control the procedures of

airspace use via complex processing and comparing

ATC flight plans and radar aerial situation information.

Basic Characteristics

Simultaneous interface with AD

automated command posts up to 2

Number of simultaneously tracked aircraft up to 300

Range:

altitude, km from 0 to 45

speed, km/h from 0 to 6,000

Time of response to operator’s action, s:

radar data processing up to 2

flight plan data processing up to 6

Operation mode continuous, 24 h

Design version stationary

Krym-KE Automation System for Input,

Processing and Transmission of

ATC Flight-Plan Data at Airfields

Intended for the automatic collection and processing of

ATC flight plan data, drawing aircraft flight plans and

their transmission to AD command posts to check the

procedure of airspace use in the AD zone (area) of

responsibility.

Basic Characteristics

Simultaneous interface

with AD automated

command posts, ATC centers,

civil AFTN network

and non-automated ATC posts up to 28

Volume of:

flight plan library, flights up to 10,000

daily flight plan, flights up to 5,000

Indication of estimated aircraft

positions in real time up to 300

Number of simultaneously

indicated flight routes up to 50

Time of response to operator’s action, s up to 6

Operation mode continuous, 24 h

Design version stationary

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670

PART 4  4

AUTOMATED CONTROL SYSTEMS

AND FACILITIES

 

   !"#$

GROUP 12 FIRE CONTROL EQUIPMENT

Class 1210 Fire Control Systems,

Complete

 12   !"# $%&'" " $("' ($!')

45677 1210 89:;69<=<>:86??@A 7<79A;@

BC>685A?<D 8:E7F6;<

FUNDAMENT-E AUTOMATED

MOBILE SYSTEM

FOR ELINT UNITS AND ELEMENTS

Fundament-1E Automated System for

Elint Company Control Post

Designed to automate the collection and processing of radar

and radio emission data received from radar stations, sec-

ondary radars and IFF interrogators; cooperating elint units;

helicopter-based radar surveillance and control systems; elint

systems and transmit summarized infor-

mation to higher-level and direct users

(command and control posts), as well as

civil ATC centers.

Basic Characteristics

Simultaneous reception and processing of data provided by:

primary and secondary radars, IFF interrogators

with digital and analog output

(via 46S6-1E automatic input module) up to 5

automated command (control) posts of elint units up to 2

airborne and shipborne radar surveillance

and control systems, and elint systems up to 1

Total number of simultaneously tracked

high-threat air targets up to 200

including active jammers

(by triangulation technique) up to 15

Range of aerial situation data processing:

plane coordinates, km up to 1,600

altitude, km up to 120

speed, km/h up to 8,000

Data processing and output cycle, s 10; 5

Simultaneous data output to

higher-level and direct users

(command and control posts)

and civil ATC centers up to 3

Time into action, min 3

Operation mode continuous, 24 h

Design version self-propelled

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671

PART 4  4

AUTOMATED CONTROL SYSTEMS

AND FACILITIES

 

   !"#$

GROUP 12 FIRE CONTROL EQUIPMENT

Class 1210 Fire Control Systems,

Complete

 12   !"# $%&'" " $("' ($!')

45677 1210 89:;69<=<>:86??@A 7<79A;@

BC>685A?<D 8:E7F6;<

Fundament-2E Automated System for

Elint Battalion Command Post

Intended to automate the procedure of collection and pro-

cessing of radar and radio emission data supplied by prima-

ry radar systems, secondary radars and IFF interrogators;

subordinate and cooperating elint units; airborne and ship-

borne radar surveillance and control systems; elint systems

and transmit summarized information to higher-level and

direct users (command and control posts), as well as civil

ATC centers.

Basic Characteristics

Simultaneous reception and processing of data provided by:

primary and secondary radars, IFF interrogators

with digital and analog output

(via 46S6-1E automatic input module) up to 6

automated command (control) posts of elint units up to 6

airborne and shipborne radar surveillance

and control systems, and elint systems up to 2

Total number of simultaneously tracked

high-threat air targets up to 300

including active jammers

(by triangulation technique) up to 25

Range of aerial situation data processing:

plane coordinates, km up to 1,600

altitude, km up to 120

speed, km/h up to 8,000

Data processing and output cycle, s 10; 5

Simultaneous data output to

higher-level and direct users

(command and control posts)

and civil ATC centers up to 10

Time into action, min 3

Operation mode continuous, 24 h

Design version self-propelled

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689:;69<=<>:86??@d 4" ("!) >6_<:9Ad?<eA7F<d C:_>6=_A5A?<E _: 6

68<6b<:??@d < F:>6`A5g?@d F:;C5AF7:8 >6_<:5:F6b<:??:f:

_:=:>6 < ?68A_A?<D, F:;C5AF7:8 >6_<:9Ad?<eA7F:E >6=8A_F< _: 2

`jAA F:5<eA798: :_?:8>A;A??: 7:C>:8:k_6A;@d

CA>8::eA>A_?@d 8:=_Bc?@d :`hAF9:8, _: 300

8 9:; e<75A C:796?:8j<F:8 6F9<8?@d C:;Ad

9><6?fB5Db<:??@; ;A9:_:; _: 25

<6C6=:? :`>6`:9F< <?a:>;6b<< : 8:=_Bc?:E :`796?:8FA:

C: C5:7F:79?@; F::>_<?696;, F; _: 1600

C: 8@7:9A, F; _: 120

C: 7F:>:79<, F;/e _: 8000

l<F5 :`>6`:9F< < 8@_6e< <?a:>;6b<<, 7 10; 5

_?:8>A;A??6D 8@_6e6 <?a:>;6b<< ?6 8@cA79:Dj<E

< :`A7CAe<86A;@A 4" < "! 8::>BkA??@d 7<5 < 8 bA?9>@

BC>685A?<D f>6k_6?7F:E 68<6b<< _: 10

>A;D C><8A_A?<D 8 `:A8Bm f:9:8?:79g, ;<?. 3

Ak<; aB?Fb<:?<>:86?<D ?AC>A>@8?@E F>Bf5:7B9:e?@E

6><6?9 F:?79>BF9<8?:f: <7C:5?A?<D 76;:d:_?@E

672

PART 4  4

AUTOMATED CONTROL SYSTEMS

AND FACILITIES

 

   !"#$

GROUP 12 FIRE CONTROL EQUIPMENT

Class 1210 Fire Control Systems,

Complete

 12   !"# $%&'" " $("' ($!')

45677 1210 89:;69<=<>:86??@A 7<79A;@

BC>685A?<D 8:E7F6;<

Fundament-3E Automated System for

Elint Formation (Unit) Command Post

Intended to automate the procedure of collection

and processing of radar and radio emission data

provided by radar stations, secondary radars and IFF

interrogators; subordinate and cooperating elint

units; airborne and shipborne radar surveillance and

control systems; elint systems and transmit summa-

rized information to higher-level and direct users

(command and control posts), as well as civil ATC

centers.

Basic Characteristics

Simultaneous reception and processing of data provided by:

automated command (control)

posts of elint formations, units and elements up to 9

airborne and shipborne radar surveillance

and control systems and elint systems up to 3

Total number of simultaneously tracked

high-threat air targets up to 400

including active jammers

(by triangulation technique) up to 40

Range of aerial situation data processing:

plane coordinates, km up to 1,600

altitude, km up to 120

speed, km/h up to 8,000

Data processing and output cycle, s 10

Simultaneous data output to

higher-level and direct users

(command and control posts)

and civil ATC centers up to 7

Time into action, min 3

Operation mode continuous, 24 h

Design version self-propelled

&CVWXFJA AIFYAKD HDKCVHKLZH[LL JCVHBYBC`C W\BJKH

IHYLCKFGBL^FAJC`C ACFYLBFBL] (^HAKL)

«S\BYHVFBK-3T»

">A_?6=?6eA? _5D 689:;69<=6b<< C>:bA77:8 7`:>6 < :`-

>6`:9F< >6_<:5:F6b<:??:E < >6_<:9Ad?<eA7F:E <?a:>;6-

b<< :9 C:_e<?A??@d < 8=6<;:_AE798Bmj<d >6_<:9Ad?<eA-

7F<d 7:A_<?A?<E, e679AE < C:_>6=_A5A?<E, 68<6b<:??@d <

F:>6`A5g?@d F:;C5AF7:8 >6_<:5:F6b<:??:f: _:=:>6 < ?6-

8A_A?<D, F:;C5AF7:8 >6_<:9Ad?<eA7F:E >6=8A_F< < 8@_6-

e< :`:`jA??:E <?a:>;6b<< ?6 8@cA79:Dj<E < :`A7CAe<-

86A;@A F:;6?_?@A CB?F9@ < CB?F9@ BC>685A?<D 8::>BkA?-

?@d 7<5 < 8 bA?9>@ BC>685A?<D f>6k_6?7F:E 68<6b<<.

$ABCDBEF GHIHJKFILAKLJL

_?:8>A;A??@E C><A; < :`>6`:9F6 <?a:>;6b<<

: 8:=_Bc?:E :`796?:8FA :9:

689:;69<=<>:86??@d 4" ("!) >6_<:9Ad?<eA7F<d 7:A_<?A?<E,

e679AE < C:_>6=_A5A?<E _: 9

68<6b<:??@d < F:>6`A5g?@d F:;C5AF7:8 >6_<:5:F6b<:??:f:

_:=:>6 < ?68A_A?<D, F:;C5AF7:8 >6_<:9Ad?<eA7F:E >6=8A_F< _: 3

`jAA F:5<eA798: :_?:8>A;A??: 7:C>:8:k_6A;@d

CA>8::eA>A_?@d 8:=_Bc?@d :`hAF9:8, _: 400

8 9:; e<75A C:796?:8j<F:8 6F9<8?@d C:;Ad

9><6?fB5Db<:??@; ;A9:_:; _: 40

<6C6=:? :`>6`:9F< <?a:>;6b<< : 8:=_Bc?:E :`796?:8FA:

C: C5:7F:79?@; F::>_<?696;, F; _: 1600

C: 8@7:9A, F; _: 120

C: 7F:>:79<, F;/e _: 8000

l<F5 :`>6`:9F< < 8@_6e< <?a:>;6b<<, 7 10

_?:8>A;A??6D 8@_6e6 <?a:>;6b<< ?6 8@cA79:Dj<E

< :`A7CAe<86A;@A 4" < "! 8::>BkA??@d 7<5 < 8 bA?9>@

BC>685A?<D f>6k_6?7F:E 68<6b<< _: 7

>A;D C><8A_A?<D 8 `:A8Bm f:9:8?:79g, ;<?. 3

Ak<; aB?Fb<:?<>:86?<D ?AC>A>@8?@E F>Bf5:7B9:e?@E

6><6?9 F:?79>BF9<8?:f: <7C:5?A?<D 76;:d:_?@E

GROUP 15 AIRCRAFT AND AIRFRAME

STRUCTURAL COMPONENTS

Class 1550 Drones

 15  

 ! " #  $ %! !"

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

673

PART 4 #  4

TRAINING TARGETS )*+,-*

LISSA-M MOBILE GROUND-BASED

SYSTEM WITH STRIZH TARGET MISSILES

Intended for prelaunch preparation, launch and in-

flight monitoring of the Strizh type target missiles used

as basic simulators of typical air targets in combat

training of air defense (AD) missile system crews and

in the operational development and trials of AD missile

systems.

The Lissa-M ground-based mobile system allows for:

- single and multiple launches of target missiles;

- continuous observation and monitoring of the target

missile in flight, as well as the dispatch of radio com-

mands to correct its trajectory and maneuver;

- all-weather operation of target missiles in various cli-

matic conditions.

The system comprises:

- launch site with six launchers, which are modified

launchers of a standard base-line AD missile system;

- command post with a special shelter, accommodat-

ing a radio command transmitter station with target

missile launch and in-flight control console, standard

all-arms radars, radio and telephone communications

facilities;

- maintenance area with a test set, representing a

modified standard base-line AD missile launcher used

for prelaunch checkout of target missiles, standard

propellant components and air servicing facilities,

transporter-loaders and a mobile power generator set.

Strizh type target missiles are expendable. They are

-".!/ 01/ %!1% « -1»

%1-1451  « .»

IJKL JM JNO JPN, KQ 

M  -RO  «TU», QW-

XY N Y NY NKJQRY ZO

 QL[-[NO JPN LN KY -

Y N (\]),  [  MY K-

Y Y .

IJNUO KO  (I-) «^-)» [-

LN:

- JLO  PQNO KQ -RO;

- N [WJ    -

R, NWLM NJLQ JJ JM -

N   N;

- NPJQW _QZW -RO N KLY

LY QNMY.

` N I- NYJM:

- NM KZM, MXM K R QNY Q-

N, KPNY Q J[ RY QNY

QN [KNP \];

- KZM JP Q, MXM K Z

KPNO [  ZO JL J-

J   Q QNM KQ   -

-R, K RY [XNONY JZ-

Y ZO  K RY JN J-  aO

NMK;

- YLM KZM, MXM K O QN-

, Z KPNO Q J[ RO

QNO QN [KNP \], JM JNO -

14

TRAINING TARGETS

GROUP 15 AIRCRAFT AND AIRFRAME

STRUCTURAL COMPONENTS

Class 1550 Drones

 15  

 ! " #  $ %! !"

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

674

PART 4 #  4

TRAINING TARGETS )*+,-*

developed from basic AD

missiles, discarded due to

the expiry of their service

life. They ensure the simula-

tion of the basic perfor-

mance characteristics of

tactical and strategic

aircraft, aeroballistic and

cruise missiles.

A target missile is launched

vertically from a mobile

launcher.

The system’s special equip-

ment comprises: flares to

enhance IR emission, a

Luneberg lens to expand the

effective reflective area

(ERA), equipment to simu-

late active radio jamming

and echoes of large targets,

and an automated system to

record and assess launch

results.

The safety of the training

target employment is

ensured by its airborne self-

destruction system, which is

activated at preset time or

on receipt of a radio com-

mand, or when the missile

deviates from the desired direction by more than 33

or the yaw or roll stabilization is disturbed.

When equipped with an altimeter, the missile can fly at

low altitudes (50 to 1,000 m) to a range of 50 km at a

speed of 650 to 120 m/s.

These target missiles have no analogs in Russia, are

relatively cheap, reliable in operation and safe in

handling. They have been extensively used by the Air

Defense Forces since 1965 (the total number of target

missiles used so far approaches 11,000).

N -RO, R-

Y JN KN -

 N  NKJQY,

RY -PQ-

KLY JN  RO -

JNUO _Z.

]-R  «TU»

JKNP M -

KJ  [K MY  N-

QUM  QUNRY NO

 _QZ KY

QNMY . j K-

NMW N N-

 Y -

N LO  PL-

O NZ, _[-

LY  Y .

\Q R KNJM

 JNUO QNO Q-

N,  - NO.

` N ZP [Q-

JNM NYJM:  JM

QM * KQLM, K

^W[P JM QNLM

kI], Q Z

NY JY  P-

N [RKY Z-

O, NKNM -

 PZ  Z

KQN [.

K M R [LNM [-

NO O  NJZ N KJO  N-

,   KNO JJ,   QYJ 

QQ  QP [ +33



,   QR [K-

Z  QQ  Q.

mN   JN KNM N-

M   O N (50-1000 )  J J

50   W  650 J 120 /.

- WX LNY PN, -R

YKQWM N KO W, N-

O _QZO JUW  [K N

. j R MWM NO I`j 

1965 PJ ([X LN KNY K _ -

J -RO -  11 ML).

!67897:; <=>=?@;>A6@A?A

TNM , P 4000

` ,  1000 - 30000

(50-1000  JN)

n ,  50 - 200

T , / 1200 - 150

nNPM QN JNQYUO o]n

 JNQY N

T QNM NM  P

 JJ  \

kI], 

[NM 0,1 - 0,3

 KO ^W[P 1,5 - 2

kQZM JU

(_aaZ [KKO [)   0,8

q[ K

(J Y J Y KY N),  12 Y 0,65 Y 2,6

Basic Characteristics

Launch weight, kg 4,000

Flight altitude, m 1,000 - 30,000

(50 - 1,000 with radio altimeter)

Flight range, km 50 - 200

Flight speed, m/s 1,200 - 150

Powerplant two-rating two-component

liquid propellant rocket motor

Control autonomous, controlled

by program or ground command

ERA, m

basic missile 0.1 - 0.3

missile with Luneberg lens 1.5 - 2

Operational reliability

(trouble-free operation factor) at least 0.8

Overall dimensions

(length x diameter x wing span), m 12 x 0.65 x 2.6

GROUP 15 AIRCRAFT AND AIRFRAME

STRUCTURAL COMPONENTS

Class 1550 Drones

 15  

 ! " #  $ %! !"

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

675

PART 4 #  4

TRAINING TARGETS ()*+,)

%-() (-75

-./0 .1

2 3-

5  -

35 3/.675

28, .1 -

3 0: -

3 /--

5 38, 

; .1 <-

  8 /-

-5 -

.

>-7

>(-75 ./3-

: 1 /-

<  </

15  ?6-

2 @A> 

B-75 3 .365 .-

C215:

- 31

-7

>(-75(E;

- 31 -

7 >(-75E.

> .3656-

01, 3

 8 ?-

.08

5. -31 6-

 (6)

.31 -

<8 3.3-

8 8 .3:  63   <-

/, 31 - I ;.8 .3:8

638  8 8 .0 3

3 3 .3:.

@6 7 /3.1  78 /8 6-

38 63,  - 8.

-.:3 7, 3. 63  ; /

 <03J1 .3 ./3-

: .3;: /:  «L-(», 3 -

3 : 35.1 2 .3  7

<I383 <6.3.

-I  /3.1 <3 68-

3 7 3 60 671 </2  66,

 ; 3 /.8  3   /38 -

...

B2 <6.3 7 3J0:

-  .1 61 ) /601;

- 38 .; (/ LJ<:) .1

6301 N-> . 1,9 

;

- .30 21Q6 .1 <01 3;.1

/  >LB «».

(7  / .3 :6 < .<6.3

28 68, 3J01 <6.3 3-

/38 8 :2  2 /6-

3 <, 68 .3.831  ..

B 7 >(-75 /0 ; 

2 /<35 3/.675 78  -

:0 5.

RM-75 TARGET MISSILE

Intended to

simulate current

and prospective

air targets, train

personnel of air

defense missile

forces and opera-

tionally develop

and test AD mis-

sile systems.

The RM-75 is an

expendable train-

ing target, devel-

oped from the

basic discarded

S-75 AD missile.

It is available in

two versions:

- RM-75MV low-

altitude target

missile;

- RM-75V high-

altitude target

missile.

The RM-75 is a

two-stage missile

with a normal

aerodynamic

configuration.

The first stage

(booster) is a

solid-propellant

rocket motor with

fins; the second stage has a liquid-propellant motor

with pumped-in propellant components.

The target missile is launched from a standard ground-

based launcher in a tilted position.

Preparation of the target missile, its launch and in-flight

tracking are performed with the use of the modernized

Lisa-M ground-based mobile system, which includes

special and standard all-arms equipment.

The flight of the target missile is discontinued either by

special airborne devices in the event of yaw stabiliza-

tion disturbance, at the preset time or by a radio

command.

The special equipment of the target missile comprises:

- flares to increase IR radiation;

- passive radio reflector (Luneberg lens) to increase the

effective reflective area (ERA) to 1.9 m

;

- 21G6 radio responder to assist in the tracking of the

missile by the Kama radar systems.

The target missile and associated ground facilities can

be replenished with optional equipment, such as an

automatic recording and launching results assessment

system, jamming equipment, etc.

The target missile is far cheaper than specially developed

air targets with similar performance characteristics.

GROUP 15 AIRCRAFT AND AIRFRAME

STRUCTURAL COMPONENTS

Class 1550 Drones

 15  

 ! " #  $ %! !"

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

676

PART 4 #  4

TRAINING TARGETS ()*+,)

Basic Characteristics

Launch weight, kg:

target missile with booster 2,350

booster 1,350

Flight range, km:

RM-75MV up to 40

RM-75V 40 - 100

Flight altitude, m:

RM-75MV 50 - 500

RM-75V 1,000 - 20,000

Flight speed, m/s:

RM-75MV 200 - 650

RM-75V 350 - 1,200

Control autonomous, using program and radio command

ERA, m

basic missile 0.1 - 0.4

missile with Luneberg lens 0.2 - 1.9

Overall dimensions, m:

length with booster 10.6

length without booster 8

diameter 0.5

wing span 1.7

!4567589 :;<;=>9<?4>?=?

B31 , ::

7  6 2350

61 1350

p , :

>(-75(E . 40

>(-75E 40 - 100

E , :

>(-75(E 50 - 500

>(-75E 1000 - 20000

B , /:

>(-75(E 200 - 650

>(-75E 350 - 1200

B 631 31  :  ..1

N-> 7, 

<31 0,1 - 0,4

 /8 LJ<: 0,2 - 1,9

Q< /, :

.  6 10,6

. </ 61 8

. 0,5

/5  1,7

GROUP 15 AIRCRAFT AND AIRFRAME

STRUCTURAL COMPONENTS

Class 1550 Drones

 15  

 ! " #  $ %! !"

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

677

PART 4 #  4

TRAINING TARGETS ()*+,)

'() %!'% «»

-./0 .1 234 2

01  ./.1 -56 

3.1 7 /4

4 (74) -

3.

(<7  203:

- >?  @4 

24, 3  0 3-

04, .3 3/.@<B -

.1  4  .4 (. 5 )

34 3 .>  -

C ./ 3;

- 32  /.7 B

34  34 .>-

4 4;

-   3/.@<4 >7

()5E) 3 < ./ -

7, 3  0 177

,   14 -

31  231, 2-

07 ;

- @? 2/ F@> )5E   /,

  3 .

5 3 <B  34.1:

- 4.1 @31 @3 GH «3.» («@2»)

2-25;

-  3/.@<7 > 3(20(3;

-  <B /B 2@.31 GH «3.-

».

)5E 3(20(3 /.  2/ GMH  3(9  <

 4B.  3 B3 -

3.1  .3/31,  4 /-

@.  >2/.

!,-./-01 234356147,6757

O,  5841

H/4 3,  932

(, B 600

H@, 0 2 - 10

O ,  . 24

O/ 3 ,  0,5 - 6

R , / 200 - 600

51 ,  . 70

(3  B@/7, .. . 8

TCC31 34 11

(3 /3  >), 

 0 2 0,1 - 0,3

 ./0 2 . 1

 /7 U?2B 3 - 5

R.3 > CB /@01  V-60

M3 3B /@01

3 C ./ 3-5 , 5/:

 304 @4 3 - 100

 .B4 @4 100 - 300

03:

34 4 10

3.3  4, <. 2 (1 .04  / / .3@4)

B  7

R2 @31  B7

R 3.> @.1

PENIYE TRAINING TARGET SYSTEM

Intended for live firings by air

defense units and testing of air

defense missile (artillery)

systems.

The training target system

ensures:

- simulation of flight of manned

and pilotless air attack assets,

including precision-guided ones,

at low and medium altitudes (up

to 5 km) in radar and infrared

bands;

- ejection of heat and passive

radar decoys in compliance with

a preset program;

- flight of an air target simulator

within a wide range of trajecto-

ries, including straight flight,

dive and pullup, as well as a bal-

listic trajectory;

- complete safety of operation of

the air target simulator on the ground and in flight.

The training target system comprises:

- 2P25 self-propelled launcher of the Kvadrat (Kub) air

defense missile system;

- 3M20M3 air target simulator;

- standard ground support equipment of the Kvadrat air

defense missile system.

The 3M20M3 air target simulator is based on the type

3M9 SAM with expired terms of serviceability, faulty

homing heads and radio fuzes, whose repair is ham-

pered or not expedient.

Basic Characteristics

Length, mm 5,841

Wing span, mm 932

Weight, kg 600

Service life, h 2 - 10

Flight range, km up to 24

Flight altitude, km 0.5 - 6

Flight speed, m/s 200 - 600

Flight time, s up to 70

G-load up to 8

ERA (depending on complement), m

with metal fairing 0.1 - 0.3

with radiotransparent fairing up to 1

with Luneberg lens 3 - 5

Infrared radiation simulation means T-60 tracking flare

Level of heat radiation

in infrared band of 3 - 5 u, W/sr:

head-on course 3 - 100

pursuit course 100 - 300

Number of:

heat decoys 10

decoy firings 2 (in train or in salvo)

flight programs 7

Flight control method programmable

Elimination method forced