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러시아 KA 29 병력수송형 헬기 로켓탄 장착모습

Summary: 러시아 KA 29 병력수송형 헬기 로켓탄 장착모습 KA 27 Helix 대잠용 헬기를 16명의 병력 수송이 가능하도록 만든 KA 29 수송형헬기는 7 62 mm MG 기관총 1문 30 mm 기관포 1문과 55mm 로켓탄발사기포드 혹은 4기의 대전차미사일등을 장착할 수 있습니다 사진은 로켓탄을 장착하고 KA 50과 훈련을 하는 모습입니다 In 1973 in response to a Navy requirement the OKB started the design and construction of a transport attack derivative of the Ka 27 the Ka 29 shipboard helicopter Deputy Chief Designer S N Fomin was entrusted with heading the design effort Leading designer G M Danilochkin became his assistant while B V Barshevsky was appointed leading engineer of the test programme The prototype made its first flight on July 28 1976 with test pilot Ye I Laryushin at the controls The Ka 29 enhanced the mobility and effectiveness of amphibious landing operations deploying both on ships and at coastal bases The helicopter featured an effective navigation targeting and communication suite Its armament in the Ka 29TB assault version comprised anti tank guided missiles gun pods unguided rockets free fall bombs and submunitions dispensers The transport version could accomodate 16 fully armed troops or carry outsize loads weighing up to 4000kg on a sling and was armed with a rapid firing 7 62 mm machine gun The State acceptance trials were completed in May 1979 and production began in 1984 In the world helicopter design practice there is no direct equivalent to the Ka 29 The 櫛 axial helicopter s ease of piloting coupled with the low vibration level lessen targeting errors and the initial dispersal of ammunition which considerably improves firing accuracy This has been substantiated by comparing the test results of the single rotor Mi 24 and the 櫛 axial Ka 29 equipped with the same models of sights fixed gun armament and unguided rockets Weapon accuracy on the Ka 29 proved to be approximately twice as high In 1987 G M Danilochkin was awarded the State Prize for his role in the development of the Ka 29 s weapons systemDeveloped for AV MF following cancellation of proposed joint service tandem rotor multirole V 50 and its replacement by what became Ka 50 meeting Army requirement only Ka 252TB prototype also known as Izdelie D2B or Izdelie 502 first flew 28 July 1976 possibly with Ka 25 nose or original narrow Ka 27 Ka 32 nose Production at Kumertau KAPP from 1984 Entered service with Northern and Pacific Fleets 1985 photographed on board assault ship Ivan Rogov in Mediterranean 1987 thought to be Ka 27B and given NATO reporting name Helix B identified as Ka 29 combat transport at Frunze Khodinka Air Show Moscow August 1989 Ka 31 radar picket version completed initial shipboard trials on aircraft carrier Admiral of the Fleet Kuznetsov then Tbilisi 1990 CURRENT VERSIONS Ka 29TB Helix B Armed derivative for day night VFR and IFR transport and close support of seaborne assault troops in the field conversion from one role to the other Non retractable landing gear and 50cm wider armoured flight deck Reportedly used by Experimental Combat Group in Chechen War in 1996 No recent production known Detailed description generally as for Ka 32 except as under Ka 31 formerly Ka 29RLD radiolokatsyonnogo Dozora radar picket helicopter Development began 1980 first flown October 1987 two examples 031 and 032 tested on Admiral of the Fleet Kuznetsov state testing completed in 1996 limited production launched for Indian Navy at Kumertau Aircraft Plant Bashkiriya 1999 Indian aircraft have 12 channel Kronshtadt GPS with Abris digital moving map and a 152x203mm AMLCD screen Basic airframe of Ka 27 with broader flight deck E 801 or E 801M export Oko eye early warning radar system by Radio Engineering Institute Nizhny Novgorod includes large rotating radar antenna area 6 0m2 that stows flat against underfuselage and deploys downward turning through 90 into vertical plane before starting to rotate at 6 rpm landing gear retracts upward to prevent interference nosewheels into long fairings Once system has been switched on antenna extended and operation mode selected data on air targets flying below helicopter뭩 altitude and on water surface situation are acquired evaluated and transmitted automatically to command centre requiring only two crew pilot and navigator latter monitoring but not operating the system in helicopter Kronshtadt Kabris GPS navigation and display system Loiter speed 100 to 120km h at up to 3 500m loiter duration 2h 30 min Maximum surveillance radius 100 to 150km for fighter size targets 250km for surface vessels up to 20 targets tracked simultaneously Antenna can be retracted manually or explosively jettisoned in the event of a forced landing Two large panniers starboard side of cabin fore and aft of main landing gear on helicopter numbered 032 forward panniers only on 031 starboard airstair type cabin door aft of flight deck divided horizontally into upward and downward opening sections with box fairing in place of window hatch window deleted above starboard rear pannier new TA 8Ka APU positioned ahove rear of engine bay fairing with slot type air intake at front of housing displacing usual ESM and IR jamming pods gives radar and antenna an independent power supply Tyre size 620x180 on main wheels 480x200 on nosewheels Tailcone extended by fairing tor flight recorder no armour guu door stores pylons or outriggers Ka 33 Utility transport Civilianised version of Ka 29TB shipborne assault transport Designation revealed tit Moscow Air Show in August 1997 no further details released and no known conversions CUSTOMERS Total of 59 Ka 29s built for Russian Federation Naval Aviation about 45 and Ukrainian Navy about 12 Following 1996 evaluation four Ka 31s ordered in August 1999 by Indian Navy for delivery in 2001 and basing aboard aircraft carriers and Krivak class destroyers further five ordered February 2001 Additional 12 maybe required Fust flight of Indian Ka 31 16 May 2001 by October 2001 first two Indian airframes delivered from KAPP to Kamov at Moscow for avionics installation flight trials completed of first two Indian aircraft by September 2002 remaining seven scheduled to follow in 2003 In October 2002 Kamov reported a second export customer for Ka 31s in addition to Indian Navy COSTS Indian Navy batch of four priced at Rs4 billion US$92 million 2000 second five cost US$108 million 2001 POWER PLANT Two Klimov TV3 117VMA turboshafts each 1 633kW Engines started by APU Fuel tanks filled with reticulated polyurethane foam for fire suppression ACCOMMODATION Wider flight deck than Ka 27 for two crew three flat plate windscreen glazings instead of two piece curved transparency 350kg of armour around cockpit and engines main cabin port side door aft of landing gear divided honzontally into upward and downward opening sections lower section forming step when open to facilitate rapid exit of up to 16 assault troops four stretcher patients seven seated casualties and medical attendant in ambulance role internal or slung cargo provisions AVIONICS Comms Two UHF and HF radios Radar Primary radar in port side of nose Flight INS Doppler box under tailboom IFF Slap Shot Mission Undernose Shturm V missile guidance and LLTV pods ESM flower pot above rear of engine bay airing Self defence L 166V IR jammer Hot Brick chaff flare dispensers EQUIPMENT Station keeping light between ESM and jammer ARMAMENT Four barrel Gatling type GShG 7 62 7 62mm machine gun with 1 800 rounds flexibly mounted behind down ward articulated door on starboard side of nose four pylons on outriggers for two four round packs of 9M114 Shturm AT 6 Spiral ASMs and two UV 32 57 57 or B 8V20 80mm rocket pods Alternative loads include four rocket packs two pods each containing a 23mm gun and 250 rounds or twn ZAB 500 incendiary bombs Internal weapons bay for torpedo or bombs Provision fur 30mm Type 2A42 gun above port outrigger with 250 round ammunition feed from cabin 러시아 KA 29 병력수송형 헬기 로켓탄 장착모습 KA 27 Helix 대잠용 헬기를 16명의 병력 수송이 가능하도록 만든 KA 29 수송형헬기는 7 62 mm MG 기관총 1문 30 mm 기관포 1문과 55mm 로켓탄발사기포드 혹은 4기의 대전차미사일등을 장착할 수 있습니다 사진은 로켓탄을 장착하고 KA 50과 훈련을 하는 모습입니다 In 1973 in response to a Navy requirement the OKB started the design and construction of a transport attack derivative of the Ka 27 the Ka 29 shipboard helicopter Deputy Chief Designer S N Fomin was entrusted with heading the design effort Leading designer G M Danilochkin became his assistant while B V Barshevsky was appointed leading engineer of the test programme The prototype made its first flight on July 28 1976 with test pilot Ye I Laryushin at the controls The Ka 29 enhanced the mobility and effectiveness of amphibious landing operations deploying both on ships and at coastal bases The helicopter featured an effective navigation targeting and communication suite Its armament in the Ka 29TB assault version comprised anti tank guided missiles gun pods unguided rockets free fall bombs and submunitions dispensers The transport version could accomodate 16 fully armed troops or carry outsize loads weighing up to 4000kg on a sling and was armed with a rapid firing 7 62 mm machine gun The State acceptance trials were completed in May 1979 and production began in 1984 In the world helicopter design practice there is no direct equivalent to the Ka 29 The 櫛 axial helicopter s ease of piloting coupled with the low vibration level lessen targeting errors and the initial dispersal of ammunition which considerably improves firing accuracy This has been substantiated by comparing the test results of the single rotor Mi 24 and the 櫛 axial Ka 29 equipped with the same models of sights fixed gun armament and unguided rockets Weapon accuracy on the Ka 29 proved to be approximately twice as high In 1987 G M Danilochkin was awarded the State Prize for his role in the development of the Ka 29 s weapons systemDeveloped for AV MF following cancellation of proposed joint service tandem rotor multirole V 50 and its replacement by what became Ka 50 meeting Army requirement only Ka 252TB prototype also known as Izdelie D2B or Izdelie 502 first flew 28 July 1976 possibly with Ka 25 nose or original narrow Ka 27 Ka 32 nose Production at Kumertau KAPP from 1984 Entered service with Northern and Pacific Fleets 1985 photographed on board assault ship Ivan Rogov in Mediterranean 1987 thought to be Ka 27B and given NATO reporting name Helix B identified as Ka 29 combat transport at Frunze Khodinka Air Show Moscow August 1989 Ka 31 radar picket version completed initial shipboard trials on aircraft carrier Admiral of the Fleet Kuznetsov then Tbilisi 1990 CURRENT VERSIONS Ka 29TB Helix B Armed derivative for day night VFR and IFR transport and close support of seaborne assault troops in the field conversion from one role to the other Non retractable landing gear and 50cm wider armoured flight deck Reportedly used by Experimental Combat Group in Chechen War in 1996 No recent production known Detailed description generally as for Ka 32 except as under Ka 31 formerly Ka 29RLD radiolokatsyonnogo Dozora radar picket helicopter Development began 1980 first flown October 1987 two examples 031 and 032 tested on Admiral of the Fleet Kuznetsov state testing completed in 1996 limited production launched for Indian Navy at Kumertau Aircraft Plant Bashkiriya 1999 Indian aircraft have 12 channel Kronshtadt GPS with Abris digital moving map and a 152x203mm AMLCD screen Basic airframe of Ka 27 with broader flight deck E 801 or E 801M export Oko eye early warning radar system by Radio Engineering Institute Nizhny Novgorod includes large rotating radar antenna area 6 0m2 that stows flat against underfuselage and deploys downward turning through 90 into vertical plane before starting to rotate at 6 rpm landing gear retracts upward to prevent interference nosewheels into long fairings Once system has been switched on antenna extended and operation mode selected data on air targets flying below helicopter뭩 altitude and on water surface situation are acquired evaluated and transmitted automatically to command centre requiring only two crew pilot and navigator latter monitoring but not operating the system in helicopter Kronshtadt Kabris GPS navigation and display system Loiter speed 100 to 120km h at up to 3 500m loiter duration 2h 30 min Maximum surveillance radius 100 to 150km for fighter size targets 250km for surface vessels up to 20 targets tracked simultaneously Antenna can be retracted manually or explosively jettisoned in the event of a forced landing Two large panniers starboard side of cabin fore and aft of main landing gear on helicopter numbered 032 forward panniers only on 031 starboard airstair type cabin door aft of flight deck divided horizontally into upward and downward opening sections with box fairing in place of window hatch window deleted above starboard rear pannier new TA 8Ka APU positioned ahove rear of engine bay fairing with slot type air intake at front of housing displacing usual ESM and IR jamming pods gives radar and antenna an independent power supply Tyre size 620x180 on main wheels 480x200 on nosewheels Tailcone extended by fairing tor flight recorder no armour guu door stores pylons or outriggers Ka 33 Utility transport Civilianised version of Ka 29TB shipborne assault transport Designation revealed tit Moscow Air Show in August 1997 no further details released and no known conversions CUSTOMERS Total of 59 Ka 29s built for Russian Federation Naval Aviation about 45 and Ukrainian Navy about 12 Following 1996 evaluation four Ka 31s ordered in August 1999 by Indian Navy for delivery in 2001 and basing aboard aircraft carriers and Krivak class destroyers further five ordered February 2001 Additional 12 maybe required Fust flight of Indian Ka 31 16 May 2001 by October 2001 first two Indian airframes delivered from KAPP to Kamov at Moscow for avionics installation flight trials completed of first two Indian aircraft by September 2002 remaining seven scheduled to follow in 2003 In October 2002 Kamov reported a second export customer for Ka 31s in addition to Indian Navy COSTS Indian Navy batch of four priced at Rs4 billion US$92 million 2000 second five cost US$108 million 2001 POWER PLANT Two Klimov TV3 117VMA turboshafts each 1 633kW Engines started by APU Fuel tanks filled with reticulated polyurethane foam for fire suppression ACCOMMODATION Wider flight deck than Ka 27 for two crew three flat plate windscreen glazings instead of two piece curved transparency 350kg of armour around cockpit and engines main cabin port side door aft of landing gear divided honzontally into upward and downward opening sections lower section forming step when open to facilitate rapid exit of up to 16 assault troops four stretcher patients seven seated casualties and medical attendant in ambulance role internal or slung cargo provisions AVIONICS Comms Two UHF and HF radios Radar Primary radar in port side of nose Flight INS Doppler box under tailboom IFF Slap Shot Mission Undernose Shturm V missile guidance and LLTV pods ESM flower pot above rear of engine bay airing Self defence L 166V IR jammer Hot Brick chaff flare dispensers EQUIPMENT Station keeping light between ESM and jammer ARMAMENT Four barrel Gatling type GShG 7 62 7 62mm machine gun with 1 800 rounds flexibly mounted behind down ward articulated door on starboard side of nose four pylons on outriggers for two four round packs of 9M114 Shturm AT 6 Spiral ASMs and two UV 32 57 57 or B 8V20 80mm rocket pods Alternative loads include four rocket packs two pods each containing a 23mm gun and 250 rounds or twn ZAB 500 incendiary bombs Internal weapons bay for torpedo or bombs Provision fur 30mm Type 2A42 gun above port outrigger with 250 round ammunition feed from cabin

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