Министерство Обороны Российской Федерации - Каталог Оружие России 2000
Название: | Каталог Оружие России 2000 | |
Автор: | Министерство Обороны Российской Федерации | |
Жанр: | Справочная литература: прочее, Спецслужбы | |
Изадано в серии: | неизвестно | |
Издательство: | неизвестно | |
Год издания: | - | |
ISBN: | неизвестно | |
Отзывы: | Комментировать | |
Рейтинг: | ||
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PART 1
MISSILE SYSTEMS
1
-
!
MISSILE AND GUN ARMAMENT
ISKANDER-E
THEATER MISSILE SYSTEM
- !
&! ' « )-*»
The system is intended to use conventional warheads
for engagement of pinpoint and area targets, such as:
- hostile fire weapons (missile systems, multiple launch
rocket systems, long-range artillery pieces);
- air and antimissile defense weapons;
- fixed- and rotary-wing aircraft at airfields;
- command posts and communications nodes;
- critical civilian infrastructure facilities;
- other vital pinpoint and area targets.
The missile system ensures:
- high probability of fire mission accomplishment in
61:3.;3.46.8139= ?415@A9 64295390. (6.0123@1 04A>-10/@,
K, :.-H34?4F3.= .629--169=);
- /61:/25. >64295454;:7N34F 9 >6429546.01234F 4?4643@;
- .59.E9= 3. .O64:64A.C;
- 04A.3:3@1 >7302@ 9 7;-@ /5=;9;
- 5.831FN91 4?P102@ G6.8:.3/04F 93Q6./2670276@;
- :67G91 5.83@1 A.-46.;A163@1 9 >-4D.:3@1 E1-9.
hostile active countermeasures environments;
- high probability of failure-proof functioning of the missile during its launch preparation and in flight;
- automatic computation and input of missile flight missions by the launcher devices;
- high tactical maneuverability and strategic mobility
owing to transportability of the system vehicles by all
types of transport;
- automation of battle management of missile units and
their information support;
- long service life and ease of operation.
The Iskander-E system is equipped with a solid-propellant single-stage guided missile controlled throughout
the entire flight path and provided with a nonseparable
warhead.
.0123@F 04A>-10/ 4?1/>14-3139= ?4154F ;.:.642954:1F/259= >64295390.;
- 5@/407S 5164=234/2H ?1;420.;34G4 Q730E9439645.39=
6.012@ >69 >4:G424501 0 >7/07, . 2.081 5 >4-121;
- .524A.297/0454F 7/2.34509;
- 5@/407S 2.029462.;
- .524A.29;.E9S ?4154G4 7>6.5-139= 6.0123@A9 >4:6.;:1-139=A9 9 9C 93Q46A.E943341 4?1/>1-7.2.E99.
.012. 04A>-10/. «U/0.3:16-V» - 2516:424>-953.=, 4:34/27>136.5-=1A.= 3. 5/1F 26.1024699 >4-12., /
3142:1-=1A4F 5 >4-121 G4-4534F 7/045.= 7/2.3450.
Self-propelled launcher
6.3/>46234-;.6=8.SD.= A.N93.
Transloader
.N93. 61G-.A132. 9 21C4?/-7895.39=
Scheduled inspection
and maintenance vehicle
4A.3:34-N2.?3.= A.N93.
Command and staff vehicle
.N93. 89;314?1/>14:G424509 93Q46A.E99
Data preparation station
Basic Characteristics
Launch range, km:
maximum
minimum
Weight, kg:
missile launch
payload
launcher
Warhead
Guidance system
Chassis
Number of missiles:
on launcher
on transloader
Time to launch, min:
from highest readiness state
after march
Assigned service life, yr
Crew
Operating temperature range, °C
/012034 56768947:/9:8:
b.-H34/2H >7/0., 0A:
A.0/9A.-H3.=
A939A.-H3.=
.//., 0G:
/2.6245.= 6.012@
>4-1;34F 3.G67;09
>7/0454F 7/2.34509
d415.= 6.5-139=
280
50
3800
480
40 000
0.//123.=, 4/04-464390.SD.=, Q7G./34-;.89G.21-H3.=
.52434A3.=, 9316E9.-H3.=,
04A>-10/9671A.= / 4>2945@N1334F >64C4:9A4/29
f.//9
4-97/0454F 7/2.34501
3. 26.3/>46234-;.6=8.SD1F A.N931
g61A= >7/0. 6.012@, A93.:
9; 5@/N1F G424534/29
/ A.6N.
.;3.-7.2.E99, G6.:.
2
2
up to 4
up to 6
10
3
±50
GROUP 10 WEAPONS
Class 1055 Launchers, Rocket
and Pyrotechnic
2
2
31 ?4-11 4
31 ?4-11 16
10
3
±50
10
-.// 1055
.012341 5446781391
83
PART 1
MISSILE SYSTEMS
1
TOCHKA-U MODERNIZED
TACTICAL MISSILE SYSTEM
45678 9 98
9 78 94:9 « 9-»
The system is designed to effectively defeat critical targets in the tactical depth of the enemy battle formation.
Components:
- solid-propellant missiles with submunition warhead
and with HEF warhead;
- self-propelled launcher (SPL);
- transloader;
- transporter;
- automated test vehicle;
- maintenance vehicle;
- arsenal equipment set;
- missile and warhead containers.
The single-stage solid-propellant missile with an inseparable warhead is inertially controlled throughout its flight
path.
The self-propelled launcher determines the coordinates
of its location, performs the prelaunch preparation and
laying of a missile, computes the flight mission data
and launches the missile from a deployed fire position
with the crew staying in the cabin.
The transloader is designed to carry missiles, perform
loading and unloading operations and to mate warheads to missiles.
61I3.Z3.L13 I-[ \]]1029534A4 H46.8139[ 5.831G^9F
_1-1G 5 2.029L1/04G A-79;
- /.>4F4I3.[ H7/045.[ 7/2.3450. (D);
- 26.3/H46234-Z.6[8.JK.[ >.^93. (M);
- 26.3/H4623.[ >.^93. ();
- .524>.29Z9645.33.[ 043264-;34-9/H=2.21-;3.[ >.^93.;
- >.^93. 21F39L1/04A4 4H-102 .6/13.-;34A4 44G . 7H6.5-139[
- 9316_9.-;3.[.
.>4F4I3.[ H7/045.[ 7/2.3450. 4 ?39@3134/8, ?58B0,84-28 5-/01D, 6?5-4,028< 0E
2- 4.0> 15-0/13588 ?3,01- 8 ?35-7028< B0,8 ?58 ,ECDF
=01036.,348
. 4D.3/313;2D=8 .8.10=-=8 .-=32-409028<
up to 200
50
10 - 20
20 C3,00 200
50
10 - 20
GUIDED WARHEAD
WITH OPTICAL HOMING HEAD
!
"D "D
!%
The warhead is designed for ballistic
battlefield and theater missiles.
Components: optical homing head,
inertial unit, onboard computers,
onboard automatic control devices,
electrohydraulic or electric control actuators.
5092-:2-;02- 9,< C-,,8.18;0./8F 5-/01
1-/18;0./3@3 8 3?05-18423-1-/18;0./3@3
2-:2-;028
-413=-18/8, L,0/153@895-4,8;0./80 8,8
L,0/158;0./80 56,04D0 ?58439D.
Basic Characteristics
Firing accuracy (maximum deviation), m
Time to prepare reference data, min
&'()'*+ ,-.-/0+.1&01/1
10 - 20
15 - 20
3;23.1H .150,HCD (?5090,H230 31/,320280), =
b50=< ?39@3134/8 L1-,3234, =82.
HYDRAULIC DRIVES
AND THEIR ELEMENTS
FOR SELF-PROPELLED
MISSILE LAUNCHERS
10 - 20
15 - 20
E %%E
F G! E
%
!F%EF "EF
" ( ) "
The drives are designed to perform
the following operations in the automatic mode:
- jacking and leveling of SPLs on
organized and deployed sites;
- elevation of guides to an assigned
angle and their retention in position during the preparation and execution of a combat mission;
- opening of covers and hatch doors and locking of
mechanisms in the traveling position;
- control of movement of armor and automotive pieces.
5092-:2-;02D 9,< 4D?3,2028< 4 -413=-18;0./3= 5078=0 .,096EZ8F 3?05-B8>:
- 4D40I84-280 8 @358:3218534-280 [
2- ?39@3134,022DF 8 20?39@3134,022DF
?,3Z-9/-F;
- ?39]0= 2- :-9-22D> 6@3, 8 69057-280
2-?5-4, :-9-;8;
- 31/5D4-280 /5DI0/, ,E/34, ^8/.-B8< =0F-28:=34 4 ?3F3923= ?3,370288 8 95.;
- 6?5-4,0280 94870280= 3C]0/134 C53201-2/343> 8 -41315-/13523> 10F28/8.
GROUP 10 WEAPONS
Class 1055 Launchers, Rocket
and Pyrotechnic
10
,-.. 1055
-/01230 4335670280
85
PART --">
MISSILE SYSTEMS
1
-
!
MISSILE AND GUN ARMAMENT
ISKANDER-E
THEATER MISSILE SYSTEM
- !
&! ' « )-*»
The system is intended to use conventional warheads
for engagement of pinpoint and area targets, such as:
- hostile fire weapons (missile systems, multiple launch
rocket systems, long-range artillery pieces);
- air and antimissile defense weapons;
- fixed- and rotary-wing aircraft at airfields;
- command posts and communications nodes;
- critical civilian infrastructure facilities;
- other vital pinpoint and area targets.
The missile system ensures:
- high probability of fire mission accomplishment in
61:3.;3.46.8139= ?415@A9 64295390. (6.0123@1 04A>-10/@,
K, :.-H34?4F3.= .629--169=);
- /61:/25. >64295454;:7N34F 9 >6429546.01234F 4?4643@;
- .59.E9= 3. .O64:64A.C;
- 04A.3:3@1 >7302@ 9 7;-@ /5=;9;
- 5.831FN91 4?P102@ G6.8:.3/04F 93Q6./2670276@;
- :67G91 5.83@1 A.-46.;A163@1 9 >-4D.:3@1 E1-9.
hostile active countermeasures environments;
- high probability of failure-proof functioning of the missile during its launch preparation and in flight;
- automatic computation and input of missile flight missions by the launcher devices;
- high tactical maneuverability and strategic mobility
owing to transportability of the system vehicles by all
types of transport;
- automation of battle management of missile units and
their information support;
- long service life and ease of operation.
The Iskander-E system is equipped with a solid-propellant single-stage guided missile controlled throughout
the entire flight path and provided with a nonseparable
warhead.
.0123@F 04A>-10/ 4?1/>14-3139= ?4154F ;.:.642954:1F/259= >64295390.;
- 5@/407S 5164=234/2H ?1;420.;34G4 Q730E9439645.39=
6.012@ >69 >4:G424501 0 >7/07, . 2.081 5 >4-121;
- .524A.297/0454F 7/2.34509;
- 5@/407S 2.029462.;
- .524A.29;.E9S ?4154G4 7>6.5-139= 6.0123@A9 >4:6.;:1-139=A9 9 9C 93Q46A.E943341 4?1/>1-7.2.E99.
.012. 04A>-10/. «U/0.3:16-V» - 2516:424>-953.=, 4:34/27>136.5-=1A.= 3. 5/1F 26.1024699 >4-12., /
3142:1-=1A4F 5 >4-121 G4-4534F 7/045.= 7/2.3450.
Self-propelled launcher
6.3/>46234-;.6=8.SD.= A.N93.
Transloader
.N93. 61G-.A132. 9 21C4?/-7895.39=
Scheduled inspection
and maintenance vehicle
4A.3:34-N2.?3.= A.N93.
Command and staff vehicle
.N93. 89;314?1/>14:G424509 93Q46A.E99
Data preparation station
Basic Characteristics
Launch range, km:
maximum
minimum
Weight, kg:
missile launch
payload
launcher
Warhead
Guidance system
Chassis
Number of missiles:
on launcher
on transloader
Time to launch, min:
from highest readiness state
after march
Assigned service life, yr
Crew
Operating temperature range, °C
/012034 56768947:/9:8:
b.-H34/2H >7/0., 0A:
A.0/9A.-H3.=
A939A.-H3.=
.//., 0G:
/2.6245.= 6.012@
>4-1;34F 3.G67;09
>7/0454F 7/2.34509
d415.= 6.5-139=
280
50
3800
480
40 000
0.//123.=, 4/04-464390.SD.=, Q7G./34-;.89G.21-H3.=
.52434A3.=, 9316E9.-H3.=,
04A>-10/9671A.= / 4>2945@N1334F >64C4:9A4/29
f.//9
4-97/0454F 7/2.34501
3. 26.3/>46234-;.6=8.SD1F A.N931
g61A= >7/0. 6.012@, A93.:
9; 5@/N1F G424534/29
/ A.6N.
.;3.-7.2.E99, G6.:.
2
2
up to 4
up to 6
10
3
±50
GROUP 10 WEAPONS
Class 1055 Launchers, Rocket
and Pyrotechnic
2
2
31 ?4-11 4
31 ?4-11 16
10
3
±50
10
-.// 1055
.012341 5446781391
83
PART 1
MISSILE SYSTEMS
1
TOCHKA-U MODERNIZED
TACTICAL MISSILE SYSTEM
45678 9 98
9 78 94:9 « 9-»
The system is designed to effectively defeat critical targets in the tactical depth of the enemy battle formation.
Components:
- solid-propellant missiles with submunition warhead
and with HEF warhead;
- self-propelled launcher (SPL);
- transloader;
- transporter;
- automated test vehicle;
- maintenance vehicle;
- arsenal equipment set;
- missile and warhead containers.
The single-stage solid-propellant missile with an inseparable warhead is inertially controlled throughout its flight
path.
The self-propelled launcher determines the coordinates
of its location, performs the prelaunch preparation and
laying of a missile, computes the flight mission data
and launches the missile from a deployed fire position
with the crew staying in the cabin.
The transloader is designed to carry missiles, perform
loading and unloading operations and to mate warheads to missiles.
61I3.Z3.L13 I-[ \]]1029534A4 H46.8139[ 5.831G^9F
_1-1G 5 2.029L1/04G A-79;
- /.>4F4I3.[ H7/045.[ 7/2.3450. (D);
- 26.3/H46234-Z.6[8.JK.[ >.^93. (M);
- 26.3/H4623.[ >.^93. ();
- .524>.29Z9645.33.[ 043264-;34-9/H=2.21-;3.[ >.^93.;
- >.^93. 21F39L1/04A4 4H-102 .6/13.-;34A4 44G . 7H6.5-139[
- 9316_9.-;3.[.
.>4F4I3.[ H7/045.[ 7/2.3450. 4 ?39@3134/8, ?58B0,84-28 5-/01D, 6?5-4,028< 0E
2- 4.0> 15-0/13588 ?3,01- 8 ?35-7028< B0,8 ?58 ,ECDF
=01036.,348
. 4D.3/313;2D=8 .8.10=-=8 .-=32-409028<
up to 200
50
10 - 20
20 C3,00 200
50
10 - 20
GUIDED WARHEAD
WITH OPTICAL HOMING HEAD
!
"D "D
!%
The warhead is designed for ballistic
battlefield and theater missiles.
Components: optical homing head,
inertial unit, onboard computers,
onboard automatic control devices,
electrohydraulic or electric control actuators.
5092-:2-;02- 9,< C-,,8.18;0./8F 5-/01
1-/18;0./3@3 8 3?05-18423-1-/18;0./3@3
2-:2-;028
-413=-18/8, L,0/153@895-4,8;0./80 8,8
L,0/158;0./80 56,04D0 ?58439D.
Basic Characteristics
Firing accuracy (maximum deviation), m
Time to prepare reference data, min
&'()'*+ ,-.-/0+.1&01/1
10 - 20
15 - 20
3;23.1H .150,HCD (?5090,H230 31/,320280), =
b50=< ?39@3134/8 L1-,3234, =82.
HYDRAULIC DRIVES
AND THEIR ELEMENTS
FOR SELF-PROPELLED
MISSILE LAUNCHERS
10 - 20
15 - 20
E %%E
F G! E
%
!F%EF "EF
" ( ) "
The drives are designed to perform
the following operations in the automatic mode:
- jacking and leveling of SPLs on
organized and deployed sites;
- elevation of guides to an assigned
angle and their retention in position during the preparation and execution of a combat mission;
- opening of covers and hatch doors and locking of
mechanisms in the traveling position;
- control of movement of armor and automotive pieces.
5092-:2-;02D 9,< 4D?3,2028< 4 -413=-18;0./3= 5078=0 .,096EZ8F 3?05-B8>:
- 4D40I84-280 8 @358:3218534-280 [
2- ?39@3134,022DF 8 20?39@3134,022DF
?,3Z-9/-F;
- ?39]0= 2- :-9-22D> 6@3, 8 69057-280
2-?5-4, :-9-;8;
- 31/5D4-280 /5DI0/, ,E/34, ^8/.-B8< =0F-28:=34 4 ?3F3923= ?3,370288 8 95.;
- 6?5-4,0280 94870280= 3C]0/134 C53201-2/343> 8 -41315-/13523> 10F28/8.
GROUP 10 WEAPONS
Class 1055 Launchers, Rocket
and Pyrotechnic
10
,-.. 1055
-/01230 4335670280
85
PART --">
- 1
- 2
- 3
- . . .
- последняя (4) »
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