AGM-88 HARM: Perbedaan antara revisi
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{{Infobox weapon |
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| name = AGM-88 HARM<ref>{{cite web|url=http://www.fas.org/man/dod-101/sys/smart/agm-88.htm |title=AGM-88 HARM (high-speed antiradiation missile) - Smart Weapons |publisher=Fas.org |date= |accessdate=2010-02-16| archiveurl= http://web.archive.org/web/20100210095535/http://www.fas.org/man/dod-101/sys/smart/agm-88.htm| archivedate= 10 February 2010 <!--DASHBot-->| deadurl= no}}</ref> |
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| image = [[File:AGM-88 HARM on FA-18C.jpg|300px]] |
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| caption = An AGM-88 HARM missile loaded aboard an F/A-18C |
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| origin = United States |
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| type = [[Air-to-surface missile|Air-to-surface]] [[anti-radiation missile]] |
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<!-- Type selection --> |
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| is_ranged = |
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| is_bladed = |
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| is_explosive = |
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| is_artillery = |
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| is_vehicle = |
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| is_missile = yes |
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| is_UK = |
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<!-- Service history --> |
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| service = 1985–present |
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| used_by = U.S. and others |
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| wars = [[Gulf War]], [[Kosovo War]], [[Iraq War]], [[2011 military intervention in Libya]] |
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<!-- Production history --> |
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| designer = [[Texas Instruments]] |
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| design_date = 1983 |
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| manufacturer = [[Texas Instruments]], then [[Raytheon Corporation]] |
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| unit_cost = {{US$|link=yes}}284,000<br>US$870,000 for AGM-88E<ref>[http://www.deagel.com/Anti-Radiation-Missiles/AGM-88E-AARGM_a001155005.aspx AGM-88E AARGM / Advanced Anti-Radiation Guided Missile, HDAM<!-- Bot generated title -->]</ref> |
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| production_date = 1983–present |
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| number = |
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| variants = |
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<!-- General specifications --> |
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| spec_label = |
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| weight = {{convert|355|kg|lb}} |
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| length = {{convert|4.1|m|ft}} |
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| part_length = |
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| width = |
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| height = |
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| diameter = {{convert|254|mm|in}} |
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| crew = |
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<!-- Ranged weapon specifications --> |
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| cartridge = |
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| caliber = |
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| barrels = |
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| action = |
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| rate = |
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| velocity = |
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| range = |
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| max_range = |
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| feed = |
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| sights = |
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<!-- Artillery specifications --> |
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| breech = |
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| recoil = |
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| carriage = |
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| elevation = |
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| traverse = |
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<!-- Bladed weapon specifications --> |
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| blade_type = |
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| hilt_type = |
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| sheath_type = |
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| head_type = |
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| haft_type = |
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<!-- Explosive specifications --> |
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| filling = WDU-21/B blast-fragmentation in a WAU-7/B warhead section, and later WDU-37/B blast-framentation warhead. |
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| filling_weight = {{convert|66|kg|lb}} |
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| detonation = FMU-111/B laser proximity fuze |
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| yield = |
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<!-- Vehicle/missile specifications --> |
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| armour = |
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| primary_armament = |
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| secondary_armament = |
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| engine = [[Thiokol]] SR113-TC-1 dual-thrust [[rocket engine]] |
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| pw_ratio = |
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| transmission = |
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| payload_capacity = |
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| suspension = |
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| clearance = |
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| wingspan = {{convert|1.1|m|ft}} |
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| propellant = Solid fuel |
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| fuel_capacity = |
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| vehicle_range = {{convert|57|nmi|mi km}} |
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| ceiling = |
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| altitude = |
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| depth = |
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| boost = |
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| speed = {{convert|2280|km/h|mph}} |
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| guidance = Passive radar homing with home-on-jam,GPS/INS and EHF active radar homing in E variant.<ref>[http://www.navair.navy.mil/index.cfm?fuseaction=home.display&key=AF4153AA-5454-44D2-B01A-AA69417C5B49 AGM-88E Advanced Anti-Radiation Guided Missile | NAVAIR - U.S. Navy Naval Air Systems Command - Navy and Marine Corps Aviation Research, Development, Acquisition, Test and Eva...<!-- Bot generated title -->]</ref> 500-20,000 MHz for AGM-88C |
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| steering = |
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| accuracy = |
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| launch_platform = [[F/A-18]], [[F-4]]G, [[F-16]], [[Tornado IDS]], [[F-35 Lightning II|F-35]] and others |
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| transport = |
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}} |
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'''AGM-88''' '''High-speed Anti-Radiation Missile''' ('''HARM''') adalah, rudal taktis udara-ke-permukaan yang dirancang di transmisi elektronik yang berasal dari sistem radar permukaan-ke-udara. Peluru kendali ini pada awalnya dikembangkan oleh Texas Instruments sebagai pengganti sistem ARM Standard RUPS-45 Shrike dan AGM-78. Produksi kemudian diambil alih oleh Perusahaan Raytheon ketika membeli bisnis produksi pertahanan Texas Instruments. |
'''AGM-88''' '''High-speed Anti-Radiation Missile''' ('''HARM''') adalah, rudal taktis udara-ke-permukaan yang dirancang di transmisi elektronik yang berasal dari sistem radar permukaan-ke-udara. Peluru kendali ini pada awalnya dikembangkan oleh Texas Instruments sebagai pengganti sistem ARM Standard RUPS-45 Shrike dan AGM-78. Produksi kemudian diambil alih oleh Perusahaan Raytheon ketika membeli bisnis produksi pertahanan Texas Instruments. |
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== Referensi == |
== Referensi == |
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{{Reflist}} |
{{Reflist}} |
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[[Kategori:Peluru kendali anti-radiasi|AGM-88 HARM]] |
[[Kategori:Peluru kendali anti-radiasi|AGM-88 HARM]] |
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[[Kategori:Raytheon|AGM-88 HARM]] |
[[Kategori:Raytheon|AGM-88 HARM]] |
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Revisi per 24 Januari 2013 12.50
| AGM-88 HARM[1] | |
|---|---|
 An AGM-88 HARM missile loaded aboard an F/A-18C | |
| Jenis | Air-to-surface anti-radiation missile |
| Negara asal | United States |
| Sejarah pemakaian | |
| Masa penggunaan | 1985–present |
| Digunakan oleh | U.S. and others |
| Pada perang | Gulf War, Kosovo War, Iraq War, 2011 military intervention in Libya |
| Sejarah produksi | |
| Perancang | Texas Instruments |
| Tahun | 1983 |
| Produsen | Texas Instruments, then Raytheon Corporation |
| Biaya produksi | US$284,000 US$870,000 for AGM-88E[2] |
| Diproduksi | 1983–present |
| Spesifikasi | |
| Berat | 355 kilogram (783 pon) |
| Panjang | 41 meter (135 ft) |
| Diameter | 254 milimeter (10,0 in) |
| Hulu ledak | WDU-21/B blast-fragmentation in a WAU-7/B warhead section, and later WDU-37/B blast-framentation warhead. |
| Hulu ledak | 66 kilogram (146 pon) |
| Mekanisme ledakan |
FMU-111/B laser proximity fuze |
| Jenis Mesin | Thiokol SR113-TC-1 dual-thrust rocket engine |
| Rentang sayap | 11 meter (36 ft) |
| Bahan bakar | Solid fuel |
| Daya jelajah | 57 mil laut (66 mi; 106 km) |
| Kecepatan | 2.280 kilometer per jam (1.420 mph) |
| Sistem pemandu |
Passive radar homing with home-on-jam,GPS/INS and EHF active radar homing in E variant.[3] 500-20,000 MHz for AGM-88C |
| Alat peluncur |
F/A-18, F-4G, F-16, Tornado IDS, F-35 and others |
AGM-88 High-speed Anti-Radiation Missile (HARM) adalah, rudal taktis udara-ke-permukaan yang dirancang di transmisi elektronik yang berasal dari sistem radar permukaan-ke-udara. Peluru kendali ini pada awalnya dikembangkan oleh Texas Instruments sebagai pengganti sistem ARM Standard RUPS-45 Shrike dan AGM-78. Produksi kemudian diambil alih oleh Perusahaan Raytheon ketika membeli bisnis produksi pertahanan Texas Instruments.
Referensi
- ^ "AGM-88 HARM (high-speed antiradiation missile) - Smart Weapons". Fas.org. Diarsipkan dari versi asli tanggal 10 February 2010. Diakses tanggal 2010-02-16.
- ^ AGM-88E AARGM / Advanced Anti-Radiation Guided Missile, HDAM
- ^ AGM-88E Advanced Anti-Radiation Guided Missile | NAVAIR - U.S. Navy Naval Air Systems Command - Navy and Marine Corps Aviation Research, Development, Acquisition, Test and Eva...