attack helicopters from different countries

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    Attack Helicopters from different countries

    Z-10

    The Z-10 attack helicopter is under development in China. It's development began in

    the mid-1990s. Prototype of the Z-10 maid it's maiden flight in 2003.

    Entered service expected in 2008 - 2009

    Crew 2 men

    Dimensions and weight

    Length 14.1 m

    Main rotor diameter 12 m

    Height 3.85

    Weight (maximum take off) 5.5 t

    Engines and performance

    Engines 2 x Pratt & Whitney PT6C-67C turboshafts

    Engine power 2 x 1 531 hp

    Maximum speed 300 km/h

    Cruising speed 250 km/h

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    Service ceiling 6 000 m

    Ferry range 800 km

    Armament

    Cannon 30-mm cannon

    Missiles HJ-9 or HJ-10 anti-tank missiles, TY-90 air-to-air missiles

    Eurocopter Tiger

    The RC 665, known in France as the Tigre and in Germany as the Tiger, was planned

    in 1984 to meet French and German requirements for an advanced multi-role type

    for battlefield operations in the typical European scenario. The Eurocopter Tiger

    attack helicopter was co-developed by France and Germany.

    Entered service 2002

    Crew 2 men

    Dimensions and weight

    Length 15.8 m

    Main rotor diameter 13 m

    Height 5.2 m

    Weight (empty) 3.3 t

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    Weight (maximum take off) 6.1 t

    Engines and performance

    Engines 2 x MTU/Turbomeca/Rolls-Royce MTR 390 turboshaft engines

    Engine power 2 x 1 285 hp

    Maximum speed 269 km/h

    Hovering ceiling 3.2 km

    Range 800 km

    Endurance 3 hours 25 minutes

    Armament

    Cannon 30-mm cannon

    Missiles 8 x HOT 2, HOT 3 or Trigat 2 anti-tank missiles; 4 x Stinger 2 or Mistral

    short-range air-to-air missiles

    Other 68 x 68-mm rockets and podded 12.7-mm guns

    Agusta A 129 Mangusta

    Conceived in response to an Italian Army requirement of the mid-1970s, the A 129

    Mangusta (Mongoose) was the first dedicated attack helicopter to be designed, built

    and deployed by a European country. Italian army operates 45 Augusta A 129

    Mangusta lightweight attack helicopters.

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    Entered service 1990

    Crew 2 men

    Dimensions and weight

    Length 14.29 m

    Main rotor diameter 11.9 m

    Weight (empty) 2.5 t

    Weight (maximum take off) 4.1 t

    Engines and performance

    Engines 2 x Piaggio (Rolls-Royce) Gem 2-2 Mk 1004D turboshaft engines

    Engine power 2 x 825 hp

    Maximum speed 259 km/h

    Combat radius 100 km

    Armament

    Cannon 1 x 20-mm cannon; can carry podded 12.7-mm machine guns

    Missiles 8 x TOW-2A anti-tank missiles

    Other 52 x 70-mm or larger 81-mm Medusa rockets

    Kawasaki OH-1

    From the mid-1980s the Japan Defence Agency (JDA), began to consider a

    successor to the OH-6D light helicopters currently in service with the Japanese

    Ground Self-Defence Force. Only 14 Kawasaki OH-1 light scout and observation

    helicopters were delivered to Japanese army.

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    Entered service 2001

    Crew 2 men

    Dimensions and weight

    Length 12 m

    Main rotor diameter 11.6 m

    Height 3.4 m

    Weight (empty) 2.4 t

    Weight (maximum take off) 4 t

    Engines and performance

    Engines 2 x Mitsubishi TS1-10 turboshafts

    Engine power 2 x 888 hp

    Maximum speed 277 km/h

    Range 550 km

    Combat radius 200 km

    Armament

    Missiles 4 x Toshiba Type 91 short-range air-to-air missiles, anti-tank missiles

    Other rocket pods

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    Mil Mi-24 Hind

    The Mi-24 Hind is one of the most widely-known assault helicopter gunships in the

    world, and remains in service with over 35 air arms.The Mi-24 Hind pack a

    formidable punch while retaining the capability to transport a squad of troops.

    Entered service 1971

    Crew 3 men

    Troops 8 men

    Dimensions and weight

    Length 19.79 m

    Main rotor diameter 17.3 m

    Height 6.5 m

    Weight (empty) 8.4 t

    Weight (maximum take off) 12.5 t

    Engines and performance

    Engines 2 x Klimov TV3-117 turboshats

    Engine power 2 x 2 200 hp

    Maximum speed 310 km/h

    Service ceiling 4.5 km/h

    Range 450 km/h

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    Combat radius 160 km

    Armament

    Cannon 1 x 4-barrel 12.7-mm gun, later replaced with a 23-mm twin-barrel cannon

    Missiles 9M17P Skorpion (AT-2 'Swatter'), 9M114 Shturm (AT-6 'Spiral')anti-tank

    guided missiles

    Other 57-mm, 80-mm, 130-mm and 240-mm rockets; AGS-17 30-mm grenade

    launchers

    Mil Mi-28 Havoc

    Despite its reported defeat by the Ka-50 Hokum, Mil received an order for a small

    batch of the Mi-28 Havoc combat helicopters from the Russian armed forces and

    continues to actively market the type. Apparently the Mil Mi-28 Havoc attack

    helicopter's design was not as successful as the Ka-50 Hokum.

    Crew 2 men

    Dimensions and weight

    Length 17 m

    Main rotor diameter 17.2 m

    Height 3.82 m

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    Weight (empty) 8.5 t

    Weight (maximum take off) 11.5 t

    Engines and performance

    Engines 2 x Klimov TV3-117VK turboshaft engines

    Engine power 2 x 2 466 hp

    Maximum speed 320 km/h

    Hovering ceiling 3.6 km

    Range 460 km

    Armament

    Cannon 1 x 30-mm cannon

    Missiles 9M114 Shturm-C, 9M120 / 9M121F Vikhr or 9A-2200 anti-tank guided

    missiles

    Kamov Ka-50 Hokum

    The Ka-50 Chernaya Akula (black shark, NATO designation Hokum) was planned as

    a rival to the Mi-28 Havoc in a competition to provide the Soviet armed forces with a

    new battlefield attack helicopter. Production of the Kamov Ka-50 Hokum attack

    helicopter is postponed with only some helicopters built.

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    Crew 1 men

    Dimensions and weight

    Length 16 m

    Main rotor diameter 14.5 m

    Height 4.93 m

    Weight (empty) 7.8 t

    Weight (maximum take off) 10.8 t

    Engines and performance

    Engines 2 x Klimov TV3-117VK turboshafts

    Engine power 2 x 2 193 hp

    Maximum speed 300 km/h

    Service ceiling 5.5 km

    Range 540 km

    Endurance 1 hour 40 minutes

    Armament

    Cannon 1 x 30-mm cannon

    Missiles 16 x 9M120 Vikhr (AT-9 'Spiral') and Vikhr-M (AT-16) anti-tank missiles

    Other ungided rockets in place of the AT missiles

    Kamov Ka-52 Hokum-B

    The Kamov Ka-52 Alligator (NATO designation Hokum-B) is a two-seat version of the

    Ka-50. It is a multi-role all-weather attack helicopter, capable operating in daytime

    and at night.

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    Crew 2 men

    Dimensions and weight

    Length 13.53 m

    Main rotor diameter 14.5 m

    Height 4.95 m

    Weight (empty) ~ 8 t

    Weight (maximum take off) 10.8 t

    Engines and performance

    Engines 2 x TV3-117VMA turboshafts

    Engine power 2 x 2 200 shp

    Maximum speed 310 km/h

    Service ceiling 5.5 km

    Range (max payload) 520 km

    Ferry range 1 200 km

    Endurance 1 hour 40 minutes

    Armament

    Cannon 1 x 30-mm cannon (460 rounds)

    Missiles 12 x Vikhr (AT-9 Spiral) anti-tank missiles / 4 x Igla-V air-to-air missiles

    Other rocket pods or bombs

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    Denel AH-2 Rooivalk

    The Atlas (now Denel) Rooivalk (red kestrel) is the first operational result of a

    development programme launched in 1981 for an indigenous attack helicopter. The

    programme initially involved the XH-1 Alpha and XTP-2 Beta as concept-proving and

    systems test-beds.The South African air forces operate only 12 Denel AH-2 Rooivalk

    attack helicopters.

    Entered service 1999

    Crew 2 men

    Dimensions and weight

    Length 18.73 m

    Main rotor diameter 15.58 m

    Height 5.19 m

    Weight (empty) 5.9 t

    Weight (maximum take off) 8.7 t

    Engines and performance

    Engines 2 x Atlas Topaz turboshaft engines

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    Engine power 2 x 2 000 hp

    Maximum cruising speed 309 km/h

    Range 940 km

    Armament

    Cannon 1 x 20-mm Armscor cannon

    Missiles 4 x four-round launchers for TOW or Denel ZT-6 Makopa anti-tank missiles,

    provision for air-to-air missiles

    Other launchers with 70-mm unoperated rockets in place of the missiles.

    OH-58 Kiowa

    Developed from the civil Bell Model 206A JetRanger helicopter, the US Army's OH-58

    Kiowa served extensively in Vietnam in the light observation and scout roles. The

    Model 206 was built in significant numbers for military service and remains in

    widespread use with the US Army in upgraded OH-58C form.

    Entered service 1969

    Crew 2 men

    Dimensions and weight

    Length 12.58 m

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    Main rotor diameter 10.67 m

    Height 3.93 m

    Weight (empty) 1.4 t

    Weight (maximum take off) 2.4 t

    Engines and performance

    Engines 1 x Allison T703-AD-700 turboshaft

    Engine power 650 hp

    Maximum speed 247 km/h

    Range 413 km

    Armament

    Missiles 4 x FIM-92 Stinger or AGM-114 Hellfire missiles

    Other 2 x 70-mm Hydra 70 rocket launchers in place of the missiles

    AH-1 HueyCobra

    In 7 September 1965 Bell flew the prototype of the world's first dedicated attack

    helicopter. Based on the Model 204 utility helicopter, the Model 209 introduced a

    new slim fuselage with a fighter-type cockpit. The pilot sits high in the rear with a

    co-pilot/gunner lower in the front directing the fire of a wide range of weapons

    mounted on lateral stub wings or under the nose. The AH-1G HueyCobra went into

    production in 1966 and over 1 000 were delivered in the first four years. The AH-1G

    saw extensive service in Vietnam.

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    Entered service 2001

    Crew 2 men

    Dimensions and weight

    Length 13.87 m

    Main rotor diameter 14.63 m

    Height 4.32 m

    Weight (empty) 4.6 t

    Weight (maximum take off) 6.69 t

    Engines and performance

    Engines 2 x General Electric T700-GE-401 turboshafts

    Engine power 2 x 1 625 hp

    Maximum speed 282 km/h

    Range 635 km

    Armament

    Cannon 1 x three-barreled 20-mm cannon

    Missiles 8 x TOW or Hellfire anti-tank missiles, AIM-9 and Stinger air-to-air missiles,

    provision for AGM-65 Maverick air-to-ground missiles

    Other various rocket pods, cluster munitions, napalm bombs

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    Boeing AH-64A Apache

    Designed in 1972 to meet the US Army's need for an AAH (Advanced Attack

    Helicopter), the AH-64A has taken over the mantle of the world's premier attack

    helicopter from the Bell AH-1 HueyCobra. The first Hughes YAH-64 prototype flew on

    30 September 1975, the programme coming under the jurisdiction of McDonnell

    Douglas from August 1985 and Boeing from 1997. The Boeing AH-64A Apache

    became the standard by which other attack helicopters are judged.

    Entered service 1986

    Crew 2 men

    Dimensions and weight

    Length 14.97 m

    Main rotor diameter 14.63 m

    Height 4.66 m

    Weight (empty) 5.1 t

    Weight (maximum take off) 9.5 t

    Engines and performance

    Engines 2 x General Electric T700-GE-701C turboshafts

    Engine power 2 x 1 800 hp

    Maximum speed 293 km/h

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    Service ceiling 6.4 km

    Range 428 km

    Armament

    Cannon 1 x 30-mm M230 cannon with 1 200 rounds

    Missiles 16 x AGM-114A Hellfire anti-tank missiles, optional AIM-9L, AIM-92A Stinger

    and Mistral air-to-air missiles, Sidearm anti-radar missile

    Other 19-shot Hydra 70 rocket pods

    Boeing AH-64D Longbow Apache

    Beginning in the late 1980s, the US Army planned a series of upgrades to its AH-64A

    fleet. The major upgrade is centred around the Northrop Grumman APG-78 Longbow

    milimetric-wavelength fire-control radar allied to new AGM-114L Hellfire 2 missiles.

    During 1992 McDonnell Douglas converted four AH-64As with this radar to act as

    proof-of-concept aircraft for a variant designated AH-64D. The Designations AH-64B

    and AH-64C for interim variants were later dropped so that the AH-64D Apache

    became the second operational Apache variant. The AH-64D Longbow Apache is

    armed with a Hellfire 2 long-range fire-and-forget ATGMs.

    Entered service 1995

    Crew 2 men

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    Dimensions and weight

    Length 14.97 m

    Main rotor diameter 14.63 m

    Height 4.9 m

    Weight (empty) 5.3 t

    Weight (maximum take off) 9.5 t

    Engines and performance

    Engines 2 x General Electric T700-GE-701C turboshafts

    Engine power 2 x 1 800 hp

    Maximum speed 265 km/h

    Service ceiling 5.9 km

    Range 407 km

    Armament

    Cannon 1 x 30-mm M230 cannon

    Missiles 16 x AGM-114L Hellfire 2 anti-tank missiles, 4 x Stinger, Mistral of 2 x AIM-

    9 Sidewinder air-to-air missiles or 2 x AGM-122 Sidearm anti-radar missiles

    Other rocket pods

    Boeing/Sikorsky RAH-66 Comanche

    The US Army's ambitious LHX (Light Helicopter Experimental) programme called for

    a new armed reconnaissance/scout helicopter to replace the service's force of 3 000

    AH-1s, OH-6s and OH-58s. A request for proposals was issued in June 1988, and 23-

    month demonstration and validation contracts were placed with two industrial

    teamings: the 'Super Team' (Bell and McDonnell Douglas) and the 'First Team'

    (Boeing and Sikorsky). In April 1991 the designation and name RAH-66 Comanche

    were selected and the First Team was announced as winner. The Comanche is

    designed for minimum observability and is based on a stealthy airframe built largely

    of composite materials. In 1998 the planned total was 1 292 helicopters with the

    possibility of 389 to be added later, however the whole programme was canceled in

    2004.

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    Crew 2 men

    Dimensions and weight

    Length 14.28 m

    Main rotor diameter 11.9 m

    Height 3.37 m

    Weight (empty) 4.06 t

    Weight (maximum take off) 7.9 t

    Engines and performance

    Engines 2 x LHTEC T800-LHT-801 turboshaft engines

    Engine power 2 x 1 432 shp

    Maximum speed 319 km/h

    Range 2 334 km (with drop tanks)

    Armament

    Cannon 1 x 20-mm three-barrel cannon in undernose turret

    Missiles up to 3 x Hellfire ATGMs or 6 x Stinger AAMs in two weapon bays or 8 x

    Hellfires / 16 x Stingers on optional stub wings

    Other Hydra-70 unoperated rocket pods in place of the missiles