SOV - 9M37M (protiletadlová raketa)

9М37М
     
Název:
Name:
9M37M 9M37M
Originální název:
Original Name:
9М37М
Kategorie:
Category:
protiletadlová řízená střela krátkého dosahu short-range air-to-air missile
Výrobce:
Producer:
DD.MM.1979-DD.MM.RRRR ?, ?
Období výroby:
Production Period:
DD.MM.1979-DD.MM.RRRR
Vyrobeno kusů:
Number of Produced:
?
Prototyp vyroben:
Prototype Built:
DD.MM.1978 (konštrukční kancelář Točmaš)
Technické údaje:
Technical Data:
 
Hmotnost střely:
Missile Weight:
39,2 kg 86 lb
Hmotnost hlavice:
Warhead Weight:
3,5 kg 8 lb
Celková délka:
Overall Length:
2190 mm 7 ft 2 ¼ in
Průměr těla:
Diameter:
120 mm 4 ¾ in
Rozpětí křídel:
Wingspan:
360 mm 1 ft 2 ⅛ in
Hlavice:
Warhead:
9N125 - třištivo-trhavá, 2,7 kg výbušniny 9N125 - High Explosive, 6 lb of explosive
Způsob navedení:
Guidance System:
pasivní samonavedení v optickém, nebo infračerveném pásmu (samonavádzací hlavice 9E47M Viraž / 9Э47М Вираж1)) Passive Homing Guidance - optical, or infrared (9E47M Virazh1))
Pohon:
Propulsion:
 
Typ:
Type:
jednostupňový raketový motor na tuhé palivo single stage solid fuel rocket engine
Výkony:
Performance:
 
Rychlost / Machovo číslo:
Speed / Mach Number:
M 1,56 (517 m/s) M 1,56 (1 696,19 ft/s)
Dosah:
Range:
52) km 32) mi
Uživatelské státy:
User States:




...




...
Poznámka:
Note:
Modifikace rakety 9M37
Použití:
- 9K35 Strela-10
- 9K35M Strela-10M
- 9K35M2 Strela-10M2
- 9K35M3 Strela-10M3
...

1) se zvýšenou odolností vůči rušení
2) min 800 m, výškový dosah 25 m - 3500 m
Modification of 9M37 missile

Used:
- 9K35 Strela-10
- 9K35M Strela-10M
- 9K35M2 Strela-10M2
- 9K35M3 Strela-10M3
...

1)with increased resistance to interference
2) min 0,49 mi, altitude from 0,015 mi to 2,17 mi
Zdroje:
Sources:
weaponsystems.net
www.militaryparitet.com
URL : https://www.valka.cz/SOV-9M37M-protiletadlova-raketa-t177147#696100 Version : 0

9M37M (STRELA-10M)




Composition of the missile: :
1 - Self-guided warhead and autopilot
2 - rudders
3 - block for rudder motors
4 - electronic block
5 - combat section
6 - non-contact igniter
7 - engine
8 - wings and ailerons
9 - tilt block
Self-guiding warhead: located in the front of the missile and is designed to intercept the target, automatically track it and give control signals. It emits an audible target acquisition signal.
It has two channels: photo-contrast (daytime), infrared (lower visibility)
Autopilot:just behind the self-guiding head.It converts the signals coming from the self-guiding head into the corresponding signals for turning the rudders.
Combat section: behind the autopilot. It is shatterproof. Designed to destroy the target.
Initiating device: It is of the non-contact type and is used to initiate the warhead when the missile strikes the target, or when it flies past the target at a distance that ensures non-contact initiation.
Composition: 1-impact igniter, in a block for steering motors.It issues a signal to the combat circuit of the fuse when the missile strikes the target.
2 - non-contact igniter, to detect an airborne target and to issue an electrical signal to the fuse combat circuit when the missile passes within an effective distance of the target.
3 - Fuse, in the combat section of the missile.Designed to provide an impulse to initiate the combat section of the missile upon receipt of a signal from the igniter.
It also ensures safe handling of the missile,when fired, until the moment of its deployment.
Engine: Produces thrust to launch the rocket and to maintain medium flight speed until the engine is shut down. Single-chamber, two-stage, solid-fuel, stable-critical nozzle cross-section with solid fuel supply and ignition device. If the missile does not hit the target,it continues to fly for 16 sec.After this time, a safety device secures the warhead and the missile does not explode when it falls to the ground.

TTU 9M37M: calibre..............120mm
missile length.....................2190mm
wingspan.................360mm
missile weight..................39.2kg
weight of missile in container.....70kg
weight of rocket with container in chest.....110kg
initiation device........contact non-contact fuse type with min. activation distance 250m from the combat vehicle
conditions of use...............-50oC to +50oC
URL : https://www.valka.cz/SOV-9M37M-protiletadlova-raketa-t177147#104243 Version : 0
something about PLRS 9M37M
- the self-guided warhead operates in two modes, photocontrast and infrared, while in the infrared channel SNH can be cooled by nitrogen, which is placed in two supershells on the rocket container, the supershells are fired by the operator and one "lasts" about 20 seconds to cool SNH.
- The non-contact igniter is optical, it works like a strobe, it is made up of four pairs of cochets displaced by 90 degrees from each other, with one being the receiving cochette and the other the transmitting one, they are set so that the reflected light beam returns to the receiving cochette at a certain distance from the target.
- from the weight of the combat load to form a 1kg explosive which is encased in pre-shaped ammunition.
- The PLRS is seized after approximately 14 to 16 seconds of flight and falls to the ground, so it is not equipped with self-destruct.
- The tilt block serves to limit the rotation of the PLRS around its long axis as much as possible, unlike the 9M32M where rotation is required.
URL : https://www.valka.cz/SOV-9M37M-protiletadlova-raketa-t177147#140388 Version : 0
Basic tactical and technical data of the 9M37M missile:


Diameter: 120 mm
Spread: 360 mm
Length: 2190 mm
Weight: 39 kg
Propulsion: single-stage solid rocket engine
Speed: max. 517 m/s
Range: effective 800-5000 m
Guidance: optical with two channels - infrared channel (single-channel infrared sensor) or photocontrast channel (cooled photocontrast PbS sensor 9E47M Virage)
Warhead: cluster-explosive, 2.7 kg explosive.
Warhead weight: 3,5 kg
Igniter: impact 9E263 and non-contact optical (four-beam) 9E347
Dimensions of the transport and firing container: 290x290x2333 mm



Source: weaponsystems.net
www.soldiering.ru
URL : https://www.valka.cz/SOV-9M37M-protiletadlova-raketa-t177147#521983 Version : 0
Gyro tracking angle of the self-guiding head....................... ± 38°
SNH sensor field of view................................................................... ± 2°
URL : https://www.valka.cz/SOV-9M37M-protiletadlova-raketa-t177147#228394 Version : 0
9M37M missile warhead
SOV - 9M37M (protiletadlová raketa) - Bočný pohľad na kontajner.

Bočný pohľad na kontajner.
SOV - 9M37M (protiletadlová raketa) - Zadná časť kontajnera rakety s gumovou krytkou.

Zadná časť kontajnera rakety s gumovou krytkou.
SOV - 9M37M (protiletadlová raketa) - Detail hlavice 9M37M

Detail hlavice 9M37M
URL : https://www.valka.cz/SOV-9M37M-protiletadlova-raketa-t177147#145355 Version : 0
Shipping crate markings and a view of them.
SOV - 9M37M (protiletadlová raketa) - Detail šablonovania na prepravných debnách rakiet.

Detail šablonovania na prepravných debnách rakiet.
SOV - 9M37M (protiletadlová raketa) - Pohľad na zatvorené debny s raketami.

Pohľad na zatvorené debny s raketami.
URL : https://www.valka.cz/SOV-9M37M-protiletadlova-raketa-t177147#146049 Version : 0
Teaching aid, cut with a missile
Brickworks 2009
SOV - 9M37M (protiletadlová raketa) - vlastní foto

vlastní foto
SOV - 9M37M (protiletadlová raketa) - vlastní foto

vlastní foto
SOV - 9M37M (protiletadlová raketa) - vlastní foto

vlastní foto
URL : https://www.valka.cz/SOV-9M37M-protiletadlova-raketa-t177147#323765 Version : 0
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