SOV - 9K310 Igla-1 [kód NATO: SA-16 Gimlet]

9K310 Игла-1
     
Název:
Name:
9K310 Igla-1 9K310 Igla-1
Originální název:
Original Name:
9K310 Игла-1
Kategorie:
Category:
přenosný protiletadlový raketový komplet s infračerveným navedením man-portable infrared homing surface-to-air missile
Výrobce:
Producer:
DD.MM.1981-DD.MM.199R KBM, Kolomna /
DD.MM.RRRR-DD.MM.RRRR ?, ?
Období výroby:
Production Period:
DD.MM.1981-DD.MM.199R
Vyrobeno kusů:
Number of Produced:
?
Prototyp vyroben:
Prototype Built:
DD.01.1980
Složení:
Composition:
 
Střela / Munice:
Missile / Ammunition:
9M313 (v raketnici 9P322)
9M313-1
Odpalovací / Palebné prostředky:
Launch / Firing Means:
9P519 (spouštěcí ústrojenství)
Prostředky velení, řízení a průzkumu:
Command, Control and Surveillance Means:
1L14 (pozemný rádiolokačný dotazovač / IFF)
1L15-1 (terminál zobrazenia situácie)
Prostředky technického zabezpečení:
Technical Support Means:
9V866
Výcvikové prostředky:
Training Means:
trenažér ?
Mobilita:
Mobility:
přenosný portable
Uživatelské státy:
User States:












































Poznámka:
Note:
Modernizace:
Igla-1M
336-24
Grom

Nelicencovaná kópie:
QW-1
Modernization:
Igla-1M
336-24
Grom

Unlicensed copy:
QW-1
Zdroje:
Sources:
http://pvo.guns.ru/pzrk/igla_01.htm
URL : https://www.valka.cz/SOV-9K310-Igla-1-kod-NATO-SA-16-Gimlet-t9096#512408 Version : 0
9K310 Igla-1


The 9K310 Igla-1 (SA-16 Gimlet) portable anti-aircraft missile system is designed to destroy low-flying targets on approach and departure, in line-of-sight conditions. It is equipped with a radio interrogator.

Compared to the PLRK Missile-3, it has a higher probability of hitting the target.

The 9M313 anti-aircraft cruise missile is equipped with a passive self-guided infrared tracking warhead.


Licensed production of the 9K310 Igla-1 set was also envisaged in Czechoslovakia. Between 1987 and 1990, production documentation and production preparation were to be carried out. Licensed production was supposed to start in 1991, but this did not happen in the end.



Technical and tactical data (PLŘS)
Rocket body diameter: 72 mm


Maximum target speed on arrival: 360 m/s (1 296 km/h)
Maximum target speed on departure: 320 m/s (1 152 km/h)


Range on arrival: 4.5 km (3.5 mi)
Range on departure: 5 km


Maximum target flight altitude: 3 000 m
Total missile weight: 10.8 kg
URL : https://www.valka.cz/SOV-9K310-Igla-1-kod-NATO-SA-16-Gimlet-t9096#107997 Version : 0

9K310 Igla-1 portable anti-aircraft kit



In the early 1970s, the Soviet Army ground forces were armed with portable anti-aircraft Strela-2 Strela-2 Strela-2 (introduced into armament in 1968), but due to the development of means of air attack against potential adversaries, it was decided by Party and government officials 12.02.12.02.12.02. 1971] to develop a new portable PL Igla complex.

The new set was defined by the following requirements:
- Increasing the resistance of the thermal homing warhead to active optical interference used by litadels and helicopters (fired flares),
- increasing the probability of target destruction in a direct hit,
- increasing the range and effectiveness of shooting targets on approach,
- ability to identify target affiliation (own/alien)
- provide advance information to individual PL gunner squads on the air situation in their area (in particular targets that are likely to be shot based on their flight characteristics).

The development of the complex was provided by the KBM Kolomna design office. In 1978, in order to accelerate the introduction of the complex into the arsenal of ground forces, it was decided to develop an "intermediate" and simplified Igla-1 complex using components (in particular, the thermal homing warhead) of the Strela-3 missile complex (06.05.1978, by the decision of the VPK No. 114).
The Igla-1 kit (Grau index 9K310) consisting of a 9M313 rocket in a 9P322 launcher, a 9P519 launcher with a 1L14 ground-based radar interrogator and a portable launcher 1L15-1 (together with the relevant technical means of control and treatment) was subjected to military trials from 15.01.1980 to 09.07.1980 at the Donguz polygon (PVO firing range). The set was included into the armament of the ground forces by the decision of the Party and the Government 1) of 11.03.1981.

Serial production of the Igla-1 kit was carried out at the Kovrov plant of V.A. Degťareva (Ковровском заводе им. В.А.Дегтярева) except for the 1L15-1 planchette, which was manufactured at the Izhevsk Electromechanical Plant (Ижевском электромеханическом заводе).

Compared to the PLRK Strela-3, the probability of destroying a F-4 type target with a single missile increased from 0.09 to 0.59 on arrival (target speed 310 m/s or 116 km/h) and from 0.07 to 0.44 on departure (target speed 260 m/s or 936 km/h). Max. values of target airspeed increased from 310 m/s to 360 m/s on arrival and from 260 m/s to 320 m/s on departure. Max. target flight altitude increased from 2200 m to 2500 m.

The improvement of the characteristics was mainly due to new technical solutions in the self-guidance system (e.g. addition of an additional circuit for the generation of control pulses just after the rocket launch to accelerate to the standard flight speed), in the rudder block (e.g. rudder control working in a new "pulse" mode, new pressure generator), as well as in the combat part. In the combat part, a higher energy explosive was used, an induction igniter was added (switching on in case of a close flyby of the target) and in case of a direct hit, the contact igniter provided, besides initiation of the combat charge, also initiation of the unconsumed fuel in the engine. To reduce aerodynamic drag, a conical aerodynamic cover ("tripod" for its mounting on 3 inclined brackets) was added in front of the thermal auto-guidance head, as well as destabilizers in a plane perpendicular to the rudders. The location of the hinged stabilizers at the rear of the rocket was also changed, allowing the rocket to be preĺlived without preĺliving the rocket tube.

To prevent the firing of "own" targets, the 1L14 recognition system was integrated into the launcher, which automatically blocked firing if a "own" recognition signal was received from the firing sector. However, since the 1L14 antenna had a diagram 30° wide in azimuth and up to 70° in bearing, it could receive the recognition signal from other own aircraft located in that sector and thus block the missile from being fired at the adversary. For such cases the fire blocking could be switched off.

The main recognition feature of the new PLRK became the truncated conical front cover of the missile launcher and the location of the power pack at an angle to the long axis of the missile launcher.

To provide information on the air situation for the pl gunner squad leader, an electronic planchette 1L15-1 was used, which was able to display the air situation (based on the received data) in a square of 25x25 km. The targets to be displayed were assigned by the superior means of the automated command system PU-12, PU-12M, PPRU-1, PPRU-1M, P-19, Kupol equipped with the ASPD-U telecoding apparatus. Information reception from PU-12M was guaranteed at a distance of min. 10 km. Relating the air situation to the specific location of the planchette was ensured by means of a compass and a map always to the given position that broadcast the situation (at that time there was no GPS yet). Planchets oriented in this way were able to show the target with an accuracy of 1000 m in range and 5°-25° in azimuth (compared to the phonic indication of targets, where the accuracy in range was up to 5 km and in azimuth up to 40°). The planchette was able to simultaneously display 4 targets with affiliation and heading markers.
The squad leader assigned targets (bearing, range, altitude) to individual gunners by voice or via radio R-147 (R-147P receivers were part of the gunner's equipment). For clear orientation, he could simultaneously gesture the appropriate direction in which the target was located.

Although the 9K310 was only a transitional solution and in the Soviet army the kit was soon supplemented by the more modern PLRK 9K38 Igla, it was exported extensively abroad and is still in use in many countries today. It has also been used successfully in several local conflicts (and civil wars, including those on the territory of the former USSR).

1) Central Committee of the Communist Party of the Soviet Union and Soviet of Ministers of the USSR (ЦК КПСС и СМ СС СР)

Source:
http://pvo.guns.ru/pzrk/igla_01.htm
http://ru.wikipedia.org/wiki
URL : https://www.valka.cz/SOV-9K310-Igla-1-kod-NATO-SA-16-Gimlet-t9096#512416 Version : 0

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

Výukový model odpalovacího zařízení přenosného protiletadlového raketového kompletu 9K310 Igla-1, Wehrtechnische Studiensammlung, Koblenz, 2009.


URL : https://www.valka.cz/SOV-9K310-Igla-1-kod-NATO-SA-16-Gimlet-t9096#379176 Version : 0
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