| tiers | |
|---|
| categories | | "WEG" |
| "Air Defense" |
| "Man-Portable Air-Defense Systems (MANPADS)" |
| "Russia (RUS)" |
| "PRO_Armenia" |
| "PRO_Belarus" |
| "PRO_Brazil" |
| "PRO_Bulgaria" |
| "PRO_Cuba" |
| "PRO_Ecuador" |
| "PRO_Egypt" |
| "PRO_Eritrea" |
| "PRO_Georgia" |
| "PRO_Hungary" |
| "PRO_India" |
| "PRO_Indonesia" |
| "PRO_Iran (Islamic Republic of)" |
| "PRO_Kazakhstan" |
| "PRO_Malaysia" |
| "PRO_Mexico" |
| "PRO_Mongolia" |
| "PRO_Morocco" |
| "PRO_Myanmar" |
| "PRO_North Korea (Democratic People's Republic of Korea)" |
| "PRO_Peru" |
| "PRO_Russian Federation" |
| "PRO_Serbia" |
| "PRO_Singapore" |
| "PRO_Slovakia" |
| "PRO_Thailand" |
| "PRO_Turkey" |
| "PRO_Ukraine" |
| "PRO_Viet Nam" |
| "PRO_Zimbabwe" |
| "Air" |
| "Tier3" |
|
|---|
| notes | "9K38 Igla (SA-18 Grouse) is a Russian-made man-portable infrared homing surface-to-air missile defense system (SAM/MANPAD). This is a third-generation, man-portable, surface-to-air missile system and it is given the Russian industrial index number 9K38, for the complete system. The SA-18 Grouse with its 9M39 missile was accepted into service in the Soviet Army in 1983.
The full-capability 9K38 Igla with its 9M39 missile was finally accepted into service in the Soviet Army in 1983. The main improvements over the Igla-1 included much-improved resistance against flares and jamming, a more sensitive seeker, expanding forward-hemisphere engagement capability to include straight-approaching fighters (all-aspect capability) under favorable circumstances, a slightly longer range, a higher-impulse, shorter-burning rocket with higher peak velocity (but the approximately same time of flight to the maximum range).
The naval variant of 9K38 Igla has the NATO reporting name SA-N-10 Grouse.
The Igla–1M missile consists of a Ground Power Supply Source (GPSS), Launching Tube, Launching Mechanism & Missile (9M 313–1).
There is also a two-barrel 9K38 missile launcher called Djigit." |
|---|
| dateOfIntroduction | 1981 |
|---|
| countryOfOrigin | "Russia (RUS)" |
|---|
| proliferation | "Armenia, Belarus, Brazil, Bulgaria, Cuba, Ecuador, Egypt, Eritrea, Georgia, Hungary, India, Indonesia, Iran (Islamic Republic of), Kazakhstan, Malaysia, Mexico, Mongolia, Morocco, Myanmar, North Korea (Democratic People's Republic of Korea), Peru, Russian Federation, Serbia, Singapore, Slovakia, Thailand, Turkey, Ukraine, Viet Nam, Zimbabwe" |
|---|
| selectedregions | |
|---|
| checkedregions | |
|---|
| checkedcountries | | "Armenia" |
| "Belarus" |
| "Brazil" |
| "Bulgaria" |
| "Cuba" |
| "Ecuador" |
| "Egypt" |
| "Eritrea" |
| "Georgia" |
| "Hungary" |
| "India" |
| "Indonesia" |
| "Iran (Islamic Republic of)" |
| "Kazakhstan" |
| "Malaysia" |
| "Mexico" |
| "Mongolia" |
| "Morocco" |
| "Myanmar" |
| "North Korea (Democratic People's Republic of Korea)" |
| "Peru" |
| "Russian Federation" |
| "Serbia" |
| "Singapore" |
| "Slovakia" |
| "Thailand" |
| "Turkey" |
| "Ukraine" |
| "Viet Nam" |
| "Zimbabwe" |
|
|---|
| dis | | name | "RUS SA18 GROUSE" |
|---|
| string | "03.01.222.011.085.022.000" |
|---|
|
|---|
| images | | "SA-18_(A).jpg" |
| "SA-18_(B).jpg" |
| "9k38IglaRUssian(A).jpg" |
|
|---|
| sections | | name | "System" |
|---|
| properties | | name | "Alternative Designation" |
|---|
| value | "9K38 Igla; NATO: SA18 Grouse" |
|---|
|
| name | "Type" |
|---|
| value | "Man-Portable Air-Defense Missile System (MANPADS)" |
|---|
|
| name | "Manufacturer" |
|---|
| value | "KB Mashinostroyeniya – Developer of the system" |
|---|
|
| name | "Family" |
|---|
| value | "9K38 Igla" |
|---|
|
| name | "Crew" |
|---|
| value | "1" |
|---|
| units | "ea" |
|---|
|
| name | "Type of Targets" |
|---|
| value | "Tactical aircraft, helicopter, UAV and cruise missile" |
|---|
|
| name | "Reaction Time" |
|---|
| value | "5-10 Seconds" |
|---|
|
| name | "Note" |
|---|
| value | "The Igla–1M missile consists of a Ground Power Supply Source (GPSS), Launching Tube, Launching Mechanism & Missile (9M 313–1)" |
|---|
|
|
|---|
|
| name | "Dimensions" |
|---|
| properties | | name | "Length, Missile" |
|---|
| value | "1.574" |
|---|
| units | "m" |
|---|
|
| name | "Diameter, Missile" |
|---|
| value | "72" |
|---|
| units | "mm" |
|---|
|
|
| name | "Weight, Combat" |
|---|
| value | "See Missile Information" |
|---|
|
|
|---|
|
| name | "Main Weapon System" |
|---|
| sections | | name | "Missile Launcher" |
|---|
| properties | | name | "Name" |
|---|
| value | "9M 313 launching mechanism" |
|---|
|
| name | "Type" |
|---|
| value | "Portable Air-Defense Missile System (MANPADS)" |
|---|
|
| name | "Note" |
|---|
| value | "There is also a two-barrel 9K38 missile launcher called Djigit" |
|---|
|
|
|---|
|
| name | "Missile" |
|---|
| properties | | name | "Name" |
|---|
| value | "9M39 Missile" |
|---|
|
| name | "Type" |
|---|
| value | "Portable Air-Defense Missile System (MANPADS)" |
|---|
|
| name | "Engine" |
|---|
| value | "Solid Fuel Rocket Motor" |
|---|
|
| name | "Length" |
|---|
| value | "1.574" |
|---|
| units | "m" |
|---|
|
| name | "Diameter" |
|---|
| value | "72" |
|---|
| units | "mm" |
|---|
|
| name | "Weight, Full System" |
|---|
| value | "17.9" |
|---|
| units | "kg" |
|---|
|
| name | "Weight, Missile" |
|---|
| value | "10.8" |
|---|
| units | "kg" |
|---|
|
| name | "Weight, Warhead" |
|---|
| value | "1.7" |
|---|
| units | "kg" |
|---|
|
| name | "Warhead Type" |
|---|
| value | "Directed-energy
blast fragmentation" |
|---|
|
| name | "Fuze Type" |
|---|
| value | "Delayed impact,
magnetic and grazing" |
|---|
|
| name | "Target Engagement" |
|---|
| value | "5,200" |
|---|
| units | "m" |
|---|
|
| name | "Speed" |
|---|
| value | "600" |
|---|
| units | "m/s" |
|---|
|
| name | "Maximum Effective Range" |
|---|
| value | "5,200" |
|---|
| units | "m" |
|---|
|
| name | "Maximum Target Speed, Receding" |
|---|
| value | "360" |
|---|
| units | "m/s" |
|---|
|
| name | "Maximum Target Speed, Approaching" |
|---|
| value | "320" |
|---|
| units | "m/s" |
|---|
|
| name | "Seeker Head Type" |
|---|
| value | "Nitrogen-cooled,
Indium antimonide (InSb)
and
uncooled lead sulfide (PbS)" |
|---|
|
| name | "Seeker Scanning" |
|---|
| value | "FM-modulated" |
|---|
|
| name | "Maximum Altitude" |
|---|
| value | "3,500" |
|---|
| units | "m" |
|---|
|
| name | "Minimum Altitude" |
|---|
| value | "10" |
|---|
| units | "m" |
|---|
|
| name | "Guidance System" |
|---|
| value | "Passive IR homing device and night vision (operating in the medium IR range)" |
|---|
|
| name | "Note" |
|---|
| value | "Missile is pitched by guidance unit over the lead point to avoid premature ground detonation when engaging targets at less than 10m. This slows engagement time." |
|---|
|
|
|---|
|
|
|---|
|
|
|---|
| variants | | name | "Igla-1E" |
|---|
| notes | "Export version." |
|---|
|
| name | "Igla-1M" |
|---|
| notes | "Improved version of 9K38 Igla. Entered service in Soviet Military during the late 1980s." |
|---|
|
| name | "Igla-1D" |
|---|
| notes | "Igla-1D" |
|---|
|
| name | "Igla-1V" |
|---|
| notes | "Air-launched version, mainly for combat helicopters." |
|---|
|
| name | "Igla-1N" |
|---|
| notes | "A version with heavier warhead at the cost of a slight reduction in range and speed." |
|---|
|
| name | "Igla-1A" |
|---|
| notes | "Export version" |
|---|
|
| name | "Strelets Igla-S / Igla" |
|---|
| notes | "The Strelets is designed for remote automated firing of the Igla and Igla-S surface-to-air missile by single shot, ripple or in salvo. In service with Syria." |
|---|
|
| name | "3M-47 Gibka" |
|---|
| notes | "A turret for ships that is equipped with Igla missiles." |
|---|
|
| name | "Komar" |
|---|
| notes | "Another turret for ships that is equipped with Igla missiles." |
|---|
|
|
|---|
| type | "WEG" |
|---|
| version | 1 |
|---|
