9K38 Igla: Perbedaan antara revisi
Tampilan
Konten dihapus Konten ditambahkan
k Bot: Perubahan kosmetika |
k Bot: Perubahan kosmetika |
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!9K38 Igla |
!9K38 Igla |
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!9K310 Igla-1 |
!9K310 Igla-1 |
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!9K338 Igla-S |
!9K338 Igla-S<ref>{{cite news|url=http://www.defensereview.com/kbm-igla-s-manpads-russian-manpackable-shoulder-launched-fire-and-forget-surface-to-air-missile-system/|title=KBM IGLA-S MANPADS: Russian Manpackable Shoulder-Launched Fire-and-Forget Surface-to-Air Missile System|deadurl=no|accessdate=14 May 2013}}</ref> |
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![[FIM-92 Stinger]] |
![[FIM-92 Stinger]] |
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Revisi per 21 Desember 2018 01.58
![](http://upload.wikimedia.org/wikipedia/commons/thumb/c/cc/IGLA-S_MANPADS_at_IDELF-2008.jpg/300px-IGLA-S_MANPADS_at_IDELF-2008.jpg)
9K38 Igla (Rusia: Игла, "jarum") adalah rudal permukaan-ke-udara (SAM) portabel homing inframerah Rusia / Soviet. "9K38" adalah penunjukan sistem Grau Rusia. Penunjukan US DoD adalah SA-18 dan pelaporan nama NATO adalah Grouse, disederhanakan, versi sebelumnya dikenal sebagai 9K310 Igla-1, atau SA-16 Gimlet.
Varian terbaru adalah 9K338 Igla-S, pelaporan nama NATO SA-24 Grinch. Telah diterjunkan oleh Angkatan Darat Rusia sejak tahun 2004.[1]
Terdapat sebuah peluncur rudal 9K38 dua barel disebut Djigit.[2]
Perbandingan dengan MANPADS lain
9K34 Strela-3 | 9K38 Igla | 9K310 Igla-1 | 9K338 Igla-S[3] | FIM-92 Stinger | |
---|---|---|---|---|---|
Service entry | 1974 | 1983 | 1981 | 2004 | 1987 |
Weight, full system, ready to shoot |
160 kg (350 pon) | 179 kg (395 pon) | 179 kg (395 pon) | 19 kg (42 pon) | 143 kg (315 pon) |
Weight, missile | 103 kg (227 pon) | 108 kg (238 pon) | 108 kg (238 pon) | 117 kg (258 pon) | 101 kg (223 pon) |
Weight, warhead | 117 kg (258 pon), 390 g (14 oz) HMX |
117 kg (258 pon), 390 g (14 oz) HMX |
117 kg (258 pon), 390 g (14 oz) HMX |
25 kg (55 pon), 585 g (20,6 oz) HMX |
2–3 kg (4,4–6,6 pon), 450 gram (16 oz) HE |
Warhead type | Directed-energy blast fragmentation |
Directed-energy blast fragmentation |
Directed-energy blast fragmentation |
Directed-energy blast fragmentation |
Annular blast fragmentation |
Fuze type | Impact and grazing fuze. | Delayed impact, magnetic and grazing. |
Delayed impact, magnetic and grazing. |
Delayed impact, magnetic and grazing. |
Delayed impact. |
Flight speed, average / peak | 470 m/s (1.100 mph) sustained | 600 m/s (1.300 mph) / 800 m/s (1.800 mph) |
570 m/s (1.300 mph) sustained (in +15 °C temperature) |
? | 700 m/s (1.600 mph) / 750 m/s (1.700 mph) |
Maximum range | 4.105 m (13.468 ft) | 5.200 m (17.100 ft) | 5.000 m (16.000 ft) | 6.000 m (20.000 ft) | 4.500 m (14.800 ft)[4] |
Maximum target speed, receding | 260 m/s (580 mph) | 360 m/s (810 mph) | 360 m/s (810 mph) | 400 m/s (890 mph) | ? |
Maximum target speed, approaching | 310 m/s (690 mph) | 320 m/s (720 mph) | 320 m/s (720 mph) | 320 m/s (720 mph) | ? |
Seeker head type | Nitrogen-cooled, lead sulfide (PbS) |
Nitrogen-cooled, Indium antimonide (InSb) and uncooled lead sulfide (PbS) |
Nitrogen-cooled, Indium antimonide (InSb) |
? | Argon-cooled, Indium antimonide (InSb) |
Seeker scanning | FM-modulated | FM-modulated | FM-modulated | FM-modulated | FM-modulated |
Seeker notes | Aerospike to reduce supersonic wave drag |
Tripod-mounted nosecone to reduce supersonic wave drag |
Referensi
Pranala luar
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