9K11 Maljutka [kód NATO: AT-3 Sagger]

9K11 Malyutka
9К11 Малютка
     
Název:
Name:
9K11 Maljutka 9K11 Malyutka
Originální název:
Original Name:
9К11 Малютка
Kategorie:
Category:
protitankový raketový komplet Anti-tank guided missile set
Výrobce:
Producer:
DD.MM.1963-DD.MM.1984 Závod V. A. Děgťarjova, Kovrov /
Období výroby:
Production Period:
DD.MM.1963-DD.MM.RRRR
Vyrobeno kusů:
Number of Produced:
?
Prototyp vyroben:
Prototype Built:
DD.MM.1962
Složení:
Composition:
 
Střela / Munice:
Missile / Ammunition:
9M14 (9М14)
9M14M
9M14M1
Odpalovací / Palebné prostředky:
Launch / Firing Means:
9P111 (9П111)
Prostředky velení, řízení a průzkumu:
Command, Control and Surveillance Means:
9S415 (9С415) so zameriavačom 9Š16 (9Ш16) (pult navedenia)
Prostředky technického zabezpečení:
Technical Support Means:
?
Výcvikové prostředky:
Training Means:
9F66A (výcvikový trenažér)
Mobilita:
Mobility:
přenosný portable
Uživatelské státy:
User States:







...







...
Poznámka:
Note:
Deriváty / kópie:
- HJ-73 Hongjian (Červený šíp 73
- RAAD
- Susong-Po
Derivate / copy:
- HJ-73 Hongjian (Red Arrow 73
- RAAD
- Susong-Po
Zdroje:
Sources:
www.russianarms.ru
www.militaryparitet.com
xn----7sbb5ahj4aiadq2m.xn--p1ai
URL : https://www.valka.cz/9K11-Maljutka-kod-NATO-AT-3-Sagger-t26808#628592 Version : 0
     
Název:
Name:
9K11 Maljutka 9K11 Malyutka
Originální název:
Original Name:
9К11 Малютка
Kategorie:
Category:
protitanková zbraň antitank weapon
Výrobce:
Producer:
Závod V. A. Děgťarjova, Kovrov / (1963-1984)
?, ? /
?, Valjevo /
Adamovské strojírny, Adamov /
Technické údaje:
Technical Data:
 
Hmotnost nenabité zbraně:
Weight Unloaded:
11,3 kg 24.91 lb
Ráže:
Calibre:
125 mm
Náboj:
Cartridge:
9M14, 9M14M
Délka:
Length:
860 mm 2 ft 9 ⅞ in
Délka hlavně:
Barrel Length:
-1) mm - 1)
Kapacita zásobníku:
Magazine Capacity:
-
Výkony:
Performance:
 
Rychlost střelby:
Rate of Fire:
4-5 ran/min 4-5 rpm
Úsťová rychlost:
Muzzle Velocity:
115 m/s 377.3 ft/s
Uživatelské státy:
User States:
Poznámka:
Note:
Kópie systému:
HJ-73 Hongjian (Červený šíp 73)
RAAD
Susong-Po


1) odpaľovacie zariadenie protitankovej riadenej strely bez hlavne
Copy of ATGM:
HJ-73 Hongjian (Red Arrow 73)
RAAD
Susong-Po


1) launcer of anti-tank missile, withouth barrel
Zdroje:
Sources:
databaza forum.valka.cz
URL : https://www.valka.cz/9K11-Maljutka-kod-NATO-AT-3-Sagger-t26808#529130 Version : 0
PTRK 9K11 Malyutka is used by the armies of more than 30 countries. It can be characterized as a medium-range PTRK with a remote guidance command system with transmission of control commands over the CLOS wire. The PTRS has the designation 9M14. Development of the Malyutka began in 1961 at the Kolomna Machine-Building Design Bureau (Konstruktorskoye bjuro machinostrojenija - KBM), and for the first time plastics were widely used in the missile's design. The Malyutka was developed in two versions, portable (designation 9A111) and mobile. The first mobile version was designated 9P110 and was based on the vehicle BRDM. Later, mobile versions 9P122 and 9P133 (with the PTRK 9M11P, the so-called Malyutka-P) were created based on the BRDM-2. The Malyutka-P already had a SACLOS guidance system with transmission of control commands over the wire. A portable version of the Malyutka was widely used during the Middle East War in October 1973, when two-man groups of Egyptian soldiers opened what looked like small suitcases and inflicted heavy casualties on Israeli tanks (over 800 Israeli tanks were hit by this missile). The missile has two engines: a starter and a main engine. The starter motor accelerates with four angled nozzles mounted just behind the warhead. The main engine has oscillating nozzle attachments that are used for steering. The missile has small wings (aerodynamic control surfaces) that fold down for infantry use. There is a stopwatch on the side. The operator can steer the missile with the naked eye up to a distance of 1000m and up to three times that distance when using binoculars. The missile weight is 10.9kg, length 860mm, diameter 125mm. The warhead is cumulative, the armour penetration is up to 400mm and the range of the missile is from 500-3000m. Versions of PTRK Malyutka: 9K11 (9M14/9M14M missile), 9K11P called Malyutka-P (9M14P), 9K11-2 Malyutka-2 (9M14-2). The anti-tank version of the BRDM-2 vehicle is equipped with a retractable six-launcher. However, the missile is now obsolete, as confirmed by the Gulf War. The PTRK was produced under license by Bulgaria and Yugoslavia. China and Iran have developed their own PTRKs based on it (Red Arrow 73 in China and RAAD and I-RAAD in Iran).

9K11 :
Range
min/max
9M14 M MALJUTKA 500/3000 m
9M14 M - P1 400/4000 m


Armour penetration at 90/60 angle

9M14 M SMALL 400/200 mm
9M14 M - P1 460/230 mm


Missile flight speed

9M14 M MALJUTKA 120 m/s
9M14 M - P1 120 m/s



Fire control system 9M14 M MALJUTKA command-by-wire
9M14 M - P1 semi-automatic (no need to control the missile
but the device must be aimed at the target)

The OZ together with one of the above missiles form the complete 9K 11
URL : https://www.valka.cz/9K11-Maljutka-kod-NATO-AT-3-Sagger-t26808#93158 Version : 0
This "first generation" PTRK is used as a portable PTRK, or forms the supplementary armament of the BMP-1 ( BVP-1), or the main armament of the BRDM "tank fighters". The set is designed, for firing at moving and non-moving armoured targets, at ranges from 500 to 3000 m. The missile control and its guidance to the target, is carried out by means of commands, transmitted to the missile by microcable, from the control pod, while simultaneously observing the missile and the target, by periscopic telescope.


The anti-tank missile set consists of: - a ground control unit and two
two launchers
- two missile boxes with markings
9M14, 9M14M, or 9M14P, P1
It is housed in three parts: - control equipment and accessories
- 9M14, 9M14M, 9M14P missiles with disconnected warheads
warheads detached
- launchers


The crew consists of three soldiers: - a senior operator (commander)
- gunner operator
- operator


The missile consists of: (a) a warhead (9H 110M) with an igniter (93212)
(b) a solid rocket motor
(c) a wing section
(d) a tracer
(e) an instrument block
(f) from the interconnecting socket


(a) The warhead shall consist of: - a body, - a cumulative cartridge, - an igniter.


The missile uses the principle of cumulative effect. The role of the missile is to 'burn through' the armour when it strikes the armour by the action of the cumulative directional beam. To initiate the cumulative charge, a contact piezoelectric igniter is used, which, after the missile is fired, is actuated at a safe distance (70 to 200 m) from the launcher. After hitting the target, the cumulative warhead of the missile is made to explode by an initiating charge from the bottom part of the missile.


(b) Rocket motor: consists of two parts: - the launcher and the propulsion motor.
The role of the launching engine is to give the missile flight speed in the shortest possible time and the role of the propulsion engine is to deliver the missile to the target.


(c) The wing section is composed of: - a body, - four wings, - a fixing device
a tracking device.

(d) Tracer: to facilitate tracking of the missile in flight.


e) The instrument block consists of: - control mechanism,- gyroscope,- coil with microcable,
- control device.


The control mechanism, gives the thruster nozzle attachments a swinging motion according to signals. The role of the gyroscope is to convey, via the microcable, to the control console, information about the angular position of the missile in flight.


The ground control equipment consists of: - a control console (9S 415),- a periscopic telescope (9Š 16), - a storage battery (11FG - 400).


The ground control device is used to launch the missile and to control it in flight by the gunner-operator, who observes the target and the missile using the periscope telescope.


The control console, by means of the control console, is used by the gunner-operator to launch the missiles which are on the launchers and to control them in flight.


The periscope telescope 9Š 16, is an optical instrument, with a magnification of 8 x and a field of view of 11 degrees 50 minutes. It is used for better observation of a flying missile.


The firing device is used to store the missile, adjust the missile's aim, fire the missile, and indicate the direction of the missile.


Missile control principle: the 9M14M, is a guided missile, with a manual command system. The missile has 4 stabilizing ailerons, designed to generate lift. The steering force is generated by deflecting the combustion gas streams, by means of swinging attachments located on the nozzles of the flight engine. In the initial phase of the missile's flight, the missile is spun up as a result of the inclined position of the thruster nozzles. On the next flight path, the rotation of the missile is maintained by the wings set at an angle of 3 degrees for 15 minutes, relative to the longitudinal axis of the missile, and by the unwinding of the connecting microcable from the spool.
In the control console, the commands (of the gunner-operator who deflects the control stick) are changed to an electrical signal. This signal, is transmitted by the connecting microcable, to the nozzle controls of the missile, which swing simultaneously to one side, away from the longitudinal axis of the missile. A single-channel control system is used to control the missile.


Guidance principle: after the shooter-operator discovers the target and aims the periscopic telescope at the target, which is within the effective firing range, the shooter-operator presses the button to fire the missile. When the missile leaves the launcher, the gunner-operator guides it to the target by keeping the centre of the threaded crosshairs of the periscopic telescope, on the target and the missile, on the target, by means of a control lever which he uses to transmit commands by means of a microcable: up, down, left, right.


Guidance: MCLOS - panel 9S415
Operation :3
Weight: 16.3 kg
Shooting speed: 4-5 shots/min.
Year of introduction: 1963
Launcher: 9A111
Weight.


Rocket designation: 9M14 MALJUTKA ,
Rocket weight: 10,9 kg
Warhead: HEAT (t) Weight: 2,5 kg.
Range:
Minimum: 500 m.
Maximum: 3000 m.
115 m./s.
400 mm.
Range to max distance : 26 s


9M14 M MALJUTKA
Rocket weight: 12,5 kg
Warhead: HEAT (t) Weight: 2,5 kg.
Range:
Minimum: 500 m.
Maximum: 3000 m.
130 m./s.
800 mm.
Range to max distance : 23 s


Guidance: SACLOS- panel 9S415/-M
Launcher: 9A111
Missile designation: 9M14 M - P1
Rocket weight: 11.4 kg
Range:
Minimum: 400 m.
Maximum: 4000 m.
115 m./s.
520 mm.
Range to max distance : 30 s
URL : https://www.valka.cz/9K11-Maljutka-kod-NATO-AT-3-Sagger-t26808#96243 Version : 0
9K11 Malyutka
is characterized by full dependence on the operator,who must track both the missile and the target throughout the missile's flight to the target. The advantage is the simple design and resistance to active jamming by the adversary. However, a significant disadvantage is the high difficulty of guiding the PTRS in realistic conditions.Another disadvantage is the low flight speed (100-180m/s).This significantly increases the time of flight to the target.A third disadvantage is the impossibility of destroying targets at short ranges up to 400-500m,because the PTRS is uncontrollable in the first phase of flight.
The probability of hitting the target is 60 to 80%

USE OF PTRS IN SETS


9M14M,9M14MK (Malyutka)
- 9K11
- BVP-1
- OT 9P133
9M14P-1-K (Malyutka)
- OT 9P133

Note: PTRS Malyutka-2 (modernized PTRK 9K11 and its modifications)
Modernization consists in installation of a new combat part,in replacement of cartridges in the starting and flight engine,in replacement of pyrotechnics. Malyutka-2 has increased effect in the target(armor penetration)and increased speed in the middle part of the flight trajectory. It can be operated on all types of standard launchers. It is shipped in standard packaging and is controlled by a standard missile control kit.
9M14M (MALJUTKA)
- Firing (destroying) at moving and non-moving armoured targets and fire assets at ranges from 500-3000m. Targets are destroyed by cumulative effect. Missile control and homing to the target is accomplished by commands relayed to the missile by microcable from the control console while simultaneously observing the missile and target.
PTRS 9M14M DESIGN:
main' parts: warhead with igniter, motor, wing section, tracer
instrument block, bottom part of missile
Warhead with igniter 9E212 :
The body is made of plastic.There is a thread in the front part for connection with the head part of the lighter. In the rear part there are two locks for connecting the warhead to the engine.In the bottom part there is a bed for the bottom part of the lighter. On the inside of the body there is a layer of silver which forms the electrical conductor.
Cumulative charge: A layer of paraffin and cerezine is applied to the lab. The cumulative charge consists of a copper cone insert, A-IX-1 explosive,insulating ring, inert foam lens.
The 9E212 igniter is of the combination type, piezoelectric with mask safety on a pyrotechnic basis with instantaneous effect (without self-destruct).(without self-destruct)
Detonation occurs at a distance of 70 to 200 m.
The main part of the igniter-(piezogenerator)forms a source of electrical energy by converting the mechanical impact energy of the projectile on the target into electrical energy.The electrical impulse obtained by compressing the piezocrystals is transferred to the bottom part of the igniter. The 16 piezo crystal spacer with a full coupling sleeve The bottom part of the lighter receives the electrical energy generated by the piezogenerator and initiates the explosive cumulative charge of the warhead.

- fusing and locking device
- pyrotechnic masking safety device
- detonating' device
- touchdown" device


Operation of head and igniter :
When the projectile is set in motion during launch, current from the ground power source is applied to the bottom part of the igniter through the touch connections.
This initiates the electric torches which ignite the delayer.In flight, the delayer burns out and its flame is transferred to the ejector cartridge, which is actuated and pulls off the fuse cap, thus making way for the fuse case, which is inserted into the case recess. The firing pin is pushed out by the spring force of the firing pin and is pushed to a stop against the wall of the housing, thereby connecting to the piezogenerator and connecting the electrospark detonator to its circuit. The fuse is inserted by spring pressure into the groove of the case, preventing the slide from bouncing backwards. This makes the fuze ready for action.When the projectile strikes the target, compression of the piezocrystals occurs. The compression produces an electric charge which is further fed to the electrospark detonator. When the appropriate voltage value is reached, a spark overcharges the insulation gap in the spark detonator, igniting the explosive component adjacent to the insulation gap.Its initiation causes the detonation of the transfer charge and thus the action charge.The cumulative charge is detonated and the armour is pierced.


Engine:
Launch motor - Gives the missile velocity(120m/s),rotation(about 50%)
Flight engine - Maintains velocity,powers the nozzle nozzle attachment controls


Wing section: body made of plastic. There are 4 protrusions on the body
(two front and two rear) for the metal' guide jaws.
four wings: made of plastic filled with foam, wing cover made of duralumin sheet, wing locking device (latch, shaft with disc, spring) stopwatch holder


stopwatch 9CH44 : - visual observation of the missile when guiding it,
body with press-fit illuminated compound, igniter and portable cap compound with electric thumbscrews with wires, Compound illuminates with red flame (2000cd) and provides visibility up to 3 km.
Instrument block: produces an information signal on the angular position of the missile,provides transmission and distribution of commands and control of nozzle attachments.


Controls nozzle attachments: distributor, gyroscope, micro-beam coil (3150m, 0.98mm diameter)


Bottom part of the missile: clamping flange, gyroscope cover, deck connection socket, rubber jacket


Igniter: Combination, impact, piezoelectric, instantaneous with mask safety, secured type, self-destructing.
Head section:(same as 9E212)
bottom part: safety and release mechanism: slide with spring
inertia sleeve with spring, 2 balancers, ignition mechanism:
trigger mechanism, pricking mechanism, inertia lock:
EIR, portable cartridge, action cartridge, inertia pin, spring
mask safety mechanism: 2 dust fuses, delay safety
detonation mechanism: self-destruct mechanism(40sec):
case, delay component, detonator, contact device
URL : https://www.valka.cz/9K11-Maljutka-kod-NATO-AT-3-Sagger-t26808#104236 Version : 0
SOV - 9K11 Maljutka / AT-3 Sagger
URL : https://www.valka.cz/9K11-Maljutka-kod-NATO-AT-3-Sagger-t26808#114823 Version : 0
taken Cihelna 2007, 18.8.2007
9K11 Maljutka [kód NATO: AT-3 Sagger] - zdroj: vlastní archív

zdroj: vlastní archív
URL : https://www.valka.cz/9K11-Maljutka-kod-NATO-AT-3-Sagger-t26808#229128 Version : 0
PTRS 9K11 Maljutka bola in the arsenal of the ČSĽA established in the year 1966.

Source : Bílek, Jiří, a. i. : the Czechoslovak people's army in the coalition ties of the Warsaw pact. MO CR 2008.
9K11 Maljutka [kód NATO: AT-3 Sagger] - Aktivácia ptrk 9K11.

Aktivácia ptrk 9K11.
URL : https://www.valka.cz/9K11-Maljutka-kod-NATO-AT-3-Sagger-t26808#252950 Version : 0

This post has not been translated to English yet. Please use the TRANSLATE button above to see machine translation of this post.

Raketa 9M14M a detail na šablónovanie (školská raketa).





URL : https://www.valka.cz/9K11-Maljutka-kod-NATO-AT-3-Sagger-t26808#312463 Version : 0
Zdroj :


Armbr. 2371/85 Anti-tank guided missile 9M14M (9M14) and 9M14P1, Description and use, 1987
URL : https://www.valka.cz/9K11-Maljutka-kod-NATO-AT-3-Sagger-t26808#371169 Version : 0
Wade

It might be worth mentioning that the czechoslovak army had pieces of czechoslovak production license. After all, even in the frames of the school of the piece are the brands -fut /Adast Adamov/.



Source :

Uzbr. 2371/85 Przeciwpancerny pocisk kierowany 9M14M (9M14) and 9M14P1, Copy and užytkowanie, 1987.
URL : https://www.valka.cz/9K11-Maljutka-kod-NATO-AT-3-Sagger-t26808#371230 Version : 0
Source: own photo
9K11 Maljutka [kód NATO: AT-3 Sagger] - Tělo motorů.

Tělo motorů.
9K11 Maljutka [kód NATO: AT-3 Sagger] - Elektromagnetické ovládání nástavců na tryskách letového RM.

Elektromagnetické ovládání nástavců na tryskách letového RM.
URL : https://www.valka.cz/9K11-Maljutka-kod-NATO-AT-3-Sagger-t26808#377207 Version : 0
the shooting 9M14M Maljutka - armament OSSR

source: miles.sk.
URL : https://www.valka.cz/9K11-Maljutka-kod-NATO-AT-3-Sagger-t26808#460820 Version : 0

Diskuse

"However, the missile is now obsolete, as the Gulf War confirmed." Now that statement would be very interesting to me... Obsolete as what? The penetration doesn't change over the years, the missile and launcher itself is basically unguaranteed (unlike others), so the only weakness is the operator himself and his abilities.
URL : https://www.valka.cz/9K11-Maljutka-kod-NATO-AT-3-Sagger-t26808#734003 Version : 0
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