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СЛУЧАЙНЫЙ КОММЕНТАРИЙ

# 978, книга: Один неловкий момент
автор: Елизавета Самонюк (Li-Catarine)

Роман "Один неловкий момент" Елизаветы Самонюк - это увлекательное путешествие любви, судьбы и последствий наших действий. Этот современный любовный роман умело сочетает остроумие с глубокими эмоциями. Сюжет вращается вокруг Арины, молодой женщины, которая пытается разобраться со своим прошлым и настоящим. После неловкого инцидента в баре она встречает загадочного Дениса. Между ними быстро вспыхивает искра, но их отношения осложняются секретами из их прошлого. Самонюк мастерски...

Министерство Обороны Российской Федерации - Каталог Оружие России 2000

Каталог Оружие России 2000
Книга - Каталог Оружие России 2000.  Министерство Обороны Российской Федерации  - прочитать полностью в библиотеке КнигаГо
Название:
Каталог Оружие России 2000
Министерство Обороны Российской Федерации

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Справочная литература: прочее, Спецслужбы

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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

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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.

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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

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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
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3. 26.3/>46234-;.6=8.SD1F A.N931
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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.

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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.

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Basic Characteristics
Firing accuracy (maximum deviation), m
Time to prepare reference data, min

&'()'*+ ,-.-/0+.1&01/1
10 - 20
15 - 20

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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.

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GROUP 10 WEAPONS
Class 1055 Launchers, Rocket
and Pyrotechnic

 10 
,-.. 1055
-/01230 4335670280

85

PART --">

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