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FOTOĞRAF VE VİDEO GALERİSİ / PHOTO AND VIDEO GALLERY => Füze, Roket ve Diğer Silah Sistemleri Galerisi / Missiles, Rockets and Other Weapons Systems Gallery => Konuyu başlatan: nightshade - 09 Şubat 2011, 17:38:47
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Güdümlü Anti Tank Füzeleri(ATGM)
AGM-114 HELLFİRE
(http://home.earthlink.net/~longbowlog1/sitebuildercontent/sitebuilderpictures/ah64d_hellfire.jpg)
(http://media.defenseindustrydaily.com/images/ORD_AGM-114K_Hellfire_II_Cutaway_Photo_lg.jpg)
Origin:United States Manufacturer:Lockheed Martin
Specifications:
Weight: 100–108lb (45.4–49kg) [1]
Length: 64 in (163 cm) Diameter: 7 in (17.8 cm)
Wingspan: 13 in (33 cm)
Warhead :High Explosive Anti-Tank (HEAT); 20 lb (9 kg) tandem anti-armor Metal augmented charge (MAC); 18 lb (8 kg) shaped-charge Blast
Engine:Solid-fuel rocket
Operational
range:500 m – 8 km
Speed: Mach 1.3 (950 mph; 425 m/s)
Guidance
system: Semi-active laser homing
millimeter wave radar seeker
Launch
platform: Rotary- and fixed-wing platforms, Unmanned combat air vehicles, tripods, ships, and ground vehicles
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MİLAN
(http://www.militarypictures.info/d/795-2/milan.jpg)
Origin:France-
West Germany
History In service: 1972–present
Used by: 41 countries Designed :1970 Manufacturer :MBDA , Bharat Dynamics (under license)
Produced: 1972
Number built: 350,000 missiles, 10,000 launchers
Variants MILAN 1, MILAN 2, MILAN 2T, MILAN 3,
MILAN ER
Specifications:
Weight: 7.1 kg
Length: 1.2 m
Diameter: 0.125 m
Wingspan: 0.26 m
Warhead: tandem HEAT Detonation
mechanism contact
Engine: solid-fuel rocket
Operational
range: 400–2000 m
Speed: 200 m/s
Guidance
system: SACLOS
Launch
platform: Individual, Vehicle
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SPİKE
(http://media.defenseindustrydaily.com/images/ORD_ATGM_Spike_Components_lg.jpg)
(http://www.deagel.com/library1/medium/m02006120900160.jpg)
Origin: Israel
History In service :1997 - Used Wars: Second Intifada, 2006 Lebanon War, War in Afghanistan (2001 –present), Gaza War
Designed:1987 Manufacturer:Rafael Advanced Defense Systems
Diehl BGT Defence (Now part of Rheinmetall Defence Electronics) Specifications: Weight
:Spike-ER from helicopter: • Missile in canister: 34 kg (74 lb 15 oz) • Launcher: 55 kg (121 lb 4 oz) • Launcher + 4 missiles: 187 kg (412 lb 4 oz) Spike-MR/LR from ground: [1] • Missile round: 14 kg (30 lb 14 oz) • Command & launch unit (CLU): 5 kg (11 lb 0 oz)
• Tripod: 2.8 kg (6 lb 3 oz) • Battery: 1 kg (2 lb 3 oz) • Thermal sight: 4 kg (8 lb 13 oz)
Length:1,670 mm (5 ft 6 in) (Missile w/ launcher) Diameter: 170 mm (6.7 in) (Missile w/launcher) Maximum range: 800 to 25,000 m depending on version Sights 10× optical sight
Warhead:Tandem-charge HEAT warhead Engine:Solid-fuel rocket Guidance
system: Infrared homing - Electro Optical (CCD, IR or Dual CCD/IIR), Passive CCD or dual CCD/IIR seeker
Spike-SR
the short range version of the
weapon, minimum range is 200 m
(660 ft) while the maximum range is
800 m (2,600 ft) and is intended for
infantry use. The reusable Command
& launch unit (CLU), battery, tripod and the thermal sight are also used
by other land-based versions (with
the exception of Spike NLOS ) of the Spike missile family, each weighing 5
kg (11 lb 0 oz), 1 kg (2 lb 3 oz), 2.8
kg (6 lb 3 oz), and 4 kg (8 lb 13 oz) respectively.[1]
Spike-MR
the medium range version. The
weight of the missile is 14 kg (30 lb
14 oz), minimum range is 200 m
(660 ft) while the maximum range is
2,500 m (8,200 ft) and is used by infantry and special forces.[6] Spike-LR long range version. The weight of
the missile is 14 kg (30 lb 14 oz),
maximum range is 4,000 m (13,000
ft) and is used by infantry and light
combat vehicles. It adds fiber-optic
communication to and from the launching soldier during flight.[7] Reported armour penetration
capability is more than 700 mm (28
in) of Rolled homogeneous armour (RHA). [8]
Spike-ER
extended range or extra long range
version of the weapon. It was
formerly also known as the NT- Dandy or NT-D. It has a maximum range of 8,000 m (26,000 ft).[9] It has a larger diameter and is heavier
than the other systems, and is
usually vehicle mounted. It is used
by infantry, LCVs , and helicopters. The Finnish Navy's Coastal Jaegers also operates the version in the anti-
ship role. The weight of the missile is
34 kg (74 lb 15 oz), the launchers
are 30 kg (66 lb 2 oz) and 55 kg
(121 lb 4 oz) respectively for the
vehicle and air-launched versions. Penetration is around 1,000 mm (39 in)
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BGM-71 TOW
(http://www.militaryfactory.com/smallarms/imgs/hughes-bgm71-tow.jpg)
Origin: United States History In service: 1970–present
Designer: Hughes Aircraft Company Designed 1963–1968
Specifications:
Length: 1.16–1.17 m (probe folded) 1.41–1.51 m (probe extended) Diameter: 0.152 m
Wingspan 0.46 m
Warhead: weight 3.9–5.9 kg
Operational
range: 3,750 m
Guidance
system: Optically-tracked, wire-guided
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UMTAS
(http://www.roketsan.com.tr/uploads/dsc01963.jpg)
(http://i267.photobucket.com/albums/ii292/cabatli_53/RoektsanUMTAS.jpg)
(http://www.defencetalk.com/pictures/data/4833/IM000695.JPG)
Origin:Turkey Manufacturer:Roketsan A.S.
Specifications:
Weight: 37.5 kg [1] Length :175 cm
Diameter: 16 cm
Warhead:
Insensitive Anti-armor Tandem
Warhead
Engine: Solid-fuel rocket
Operational
range :500 – 8000 m
Guidance
system: Imaging Infrared Seeker
Launch
platform: Rotary wing platforms
Unmanned combat air vehicles
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ERYX
(http://i16.photobucket.com/albums/b24/hybenamon/LAND/MISSILES/ERYX%20-%20FRENCH%20AT%20MISSILE/eryx-7.jpg)
Origin: France
Canada
History In service:1994 Used by:Operators Designed :1985-92 Manufacturer:MBDA Produced :1993
Specifications
Weight:16.0 kg (13.0 kg missile and container, firing post 4.0 kg)
Length:0.905 m (2.97 ft) Diameter:0.136 m (5.4 in)
WARHEAD:137 mm diameter 3.6 kg tandem HEAT (penetrating 900 mm RHA behind reactive armour[1], or 2.5 m through concrete)
Operational Range: 50–600 m
Speed 18 m/s (65 km/h ) at launch to 245 m/ s (880 km/h) at 600 m
Guidance:
system SACLOS wire Launch:
platform Individual, Vehicle
http://i16.photobucket.com/albums/b24/hybenamon/LAND/MISSILES/ERYX%20-%20FRENCH%20AT%20MISSILE/eryx-7.jpg
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FGM-148 JAVELİN
(http://media.defenseindustrydaily.com/images/ORD_ATGM_Javelin_Launch_Immediate_lg.jpg)
(http://www.strangemilitary.com/images/content/101794.jpg)
Origin:United States History In service: 1996– Users Wars Operation: Enduring Freedom (2001– present) Operation Iraqi Freedom / Operation New Dawn (2003–present)
Designer: Texas Instruments and Martin Marietta (now Raytheon and Lockheed Martin ) Designed June 1989 Manufacturer: Raytheon and Lockheed Martin
Unit cost:$40,000 (£20,000) (missile); $
125,000 (reusable Command Launch
Unit)
Specifications:
Weight: Missile- 11.8 kg (26 lb) [1] CLU: 6.4 kg (14.1 lb)
Length:Missile: 1.1 m (43 in)
Launch tube: 1.2 m (47 in)
Diameter: Missile: 127 mm (5.0 in)
Launch tube: 142 mm (5.6 in) Crew 2
Effective range: 75 to 2500 m
Warhead: Tandem shaped charge HEAT Warhead weight: 8.4 kg (18.5 lb) [2]
Engine: Solid fuel rocket
Guidance
system: Imaging infrared (IIR)
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KORNET
(http://www.defense-update.com/images/kornet-e.jpg)
(http://www.strategypage.com/gallery/images/kornet.jpg)
Origin:Russia
History In service:1994-present
Designer:KBP Instrument Design:Bureau Manufacturer:KBP Instrument
Variants: 9M123, 9M123-2, 9M123F, 9M123F-2
Specifications:
(9M133)
Weight: 27 kg (29 kg with launch tube)
Length :1200 mm Diameter :152 mm
Warhead: 1000-1200 mm RHA [1] penetration after ERA with Tandem HEAT , Thermobaric Warhead weight 7 kg HEAT, 10 kg TNT equivalent
Thermobaric
Engine: Solid-fuel rocket
Operational
range: 100-5500m
Guidance
system: SACLOS laser beam riding
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RBS 56 BILL
(http://www.rok.ee/scouts/images/gallery/XUTCCK/BILL_BE_02.jpg)
Origin: Sweden History In service: 1985-
Used by: Sweden, Austria , Lithuania, Brazil Manufacturer: Bofors Produced: 1985 - lte 1990s
Number built: 15,000 +
Specifications:
Weight: 36 kg (launcher) Length: 900 mm Diameter:150 mm
Effective range: 150 to 2,200 m
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LAHAT
(http://img689.imageshack.us/img689/2659/31358200.jpg)
Origin: Israel
Service: 1992 - present Used by: Israel, India
Unit cost $20,000 (1999)
Specifications
Weight: 13.5 kg
Length: 97.5 cm Diameter: 105 mm Warhead: Tandem HEAT Warhead weight: 4.5 kg Operational
range: 8000 m
Speed: 285-300 m/s
Guidance
system :Semi-Active Laser Homing
Launch
platform: 105 - 120 mm smooth bore
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HJ-10
(http://image01.wiki.livedoor.jp/n/2/namacha2/68716a6b0d1f9909.jpg)
Origin: China
Used by: China Manufacturer:China North Industries Group
Corporation Elctro-Opticals Science &
Technology Ltd.
Specifications
Weight ≈ 50 kg
Warhead: HEAT and others
Engine: rocket motor Propellant solid fuel Operational
range ≈ 10+ km
Speed: supersonic Guidance
system: ImIR, semi-active laser homing, TV and MMW ARH Launch
platform: Air and ground-based
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Sağlam paylaşımlar
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Sağlam paylaşımlar
katılıyorum , konu çok güzel olmuş
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Sağolun arkadaşlar, daha hazırlıyorum devam edecem.
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MATHOGO
(http://2.bp.blogspot.com/_80_yaznP3lM/TTULuzbCEzI/AAAAAAAABY0/A06P_Kokc4g/s1600/Mathogo-1.jpg)
Origin :Argentina Production history: Designed 1970's Manufacturer: CITEFA
Specifications
Weight: 11.3 kg (25 lb) Length :0.998 m (3.27 ft) Diameter: 102 mm (4.0 in)
Warhead: 2.8-kg HEAT warhead
Engine: Two-stage solid fuel rocket
Wingspan: 470 mm (19 in)
Operational
range:400-3000 m[1]
Speed :324 km/h (202 miles/hr) Guidance
system: MCLOS with wing-edge spoilers Launch
platform: vehicle, ground
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NAG
(http://www.tribuneindia.com/2008/20080715/chd1.jpg)
(http://www.thehindu.com/multimedia/dynamic/00121/06-NAG_MISSILE_TEST_121722f.jpg)
Origin:India
Service: 2009 -
Used by:India Manufacturer: Bharat Dynamics Limited (BDL) Specifications
Weight: 42 kg (93 lb) Length :1.90 m (6'3") Diameter: 190 mm (7.5 in)
Warhead: 8 kg (17.6 lb) tandem warhead
Engine :Tandem solid Propulsion
Wingspan: 400 mm Operational
range: Land version, 500m to 4km (Air launched: 7km) [1] Speed: 230 m/s Guidance
system: Active Imaging infra-red (IIR) seeker, millimetric wave (mmW) seeker (under development)
Launch
platform: Nag Missile Carrier (NAMICA)- HAL Dhruv Helicopter -HAL Light Combat Helicopter
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Arkadaşlar, bizim Umtas diğer anti tank füzeleri arasında iyi bir konumda mı?
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Arkadaşlar, bizim Umtas diğer anti tank füzeleri arasında iyi bir konumda mı?
Geliştirme , deneme aşamasında , ön görülen özelliklerine (ilk sayfada verilmiş) baktığımızda bu füzelerden geri kalmaz
isabet oranı , gerçek maliyeti , vuruş gücü , hızı ve aklıma gelmeyen birçok özelliğide tam kesinleşmedi , başarılı test atışlarını görmeden ne söylesek yalan olur.
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Sanırım en az hellfire II kadar olmasını beklemek yanlış olmaz.