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
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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
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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
URL : https://www.valka.cz/SOV-9M37M-protiletadlova-raketa-t177147#521983
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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
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9M37M missile warhead
Bočný pohľad na kontajner.
Zadná časť kontajnera rakety s gumovou krytkou.
Detail hlavice 9M37M
URL : https://www.valka.cz/SOV-9M37M-protiletadlova-raketa-t177147#145355
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Shipping crate markings and a view of them.
Detail šablonovania na prepravných debnách rakiet.
Pohľad na zatvorené debny s raketami.
URL : https://www.valka.cz/SOV-9M37M-protiletadlova-raketa-t177147#146049
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Teaching aid, cut with a missile Brickworks 2009
vlastní foto
vlastní foto
vlastní foto
URL : https://www.valka.cz/SOV-9M37M-protiletadlova-raketa-t177147#323765
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