超级军网HQ-19(S-400)在中国
来源：百度文库 编辑：超级军网 时间：2024/04/30 18:54:54
HQ-19 (S-400)：
http://www.janes.com/extracts/extract/jsws/jsws9067.html
It is now believed that the Russian S-400 Triumf (Chinese designator HQ-19) surface-to-air missile system was a joint development programme with China. The system uses the same sensors, battle management and launch vehicles as the Russian S-300 (SA-10/-20 'Grumble') and Chinese HQ-9/-15. The S-400 introduces three new missiles, the 9M96, 9M96/2 and the 40N6, which can be fitted in new canisters replacing all or some of the S-300 missile canisters on the TEL. It is believed that a new TEL vehicle has been developed specifically to carry the S-400 missiles, and that this is a wheeled vehicle carrying six to eight missiles. The 9M96 missile has a length of 4.75 m, a body diameter of 0.24 m, a launch weight of 333 kg, and a 24 kg HE warhead. Guidance is inertial with command updates and an active radar terminal seeker. The missile has a two-stage solid propellant motor system, with a maximum range of 40 km. The second stage has lateral thrust motors to improve manoeuvrability in the terminal phase, similar to the US PAC-3 design. It can intercept targets from 5 m up to 20 km altitude. The 9M96/2 missile has a length of 5.65 m, a body diameter of 0.24 m, and a launch weight of 420 kg. The two missiles share the same separating second stage, but have different boost motors. The 9M96/2 missile has a maximum range of 120 km, and can intercept targets from 5 m up to 30 km altitude. The 40N6 version
图片：
:D :DHQ-19 (S-400)：
http://www.janes.com/extracts/extract/jsws/jsws9067.html
It is now believed that the Russian S-400 Triumf (Chinese designator HQ-19) surface-to-air missile system was a joint development programme with China. The system uses the same sensors, battle management and launch vehicles as the Russian S-300 (SA-10/-20 'Grumble') and Chinese HQ-9/-15. The S-400 introduces three new missiles, the 9M96, 9M96/2 and the 40N6, which can be fitted in new canisters replacing all or some of the S-300 missile canisters on the TEL. It is believed that a new TEL vehicle has been developed specifically to carry the S-400 missiles, and that this is a wheeled vehicle carrying six to eight missiles. The 9M96 missile has a length of 4.75 m, a body diameter of 0.24 m, a launch weight of 333 kg, and a 24 kg HE warhead. Guidance is inertial with command updates and an active radar terminal seeker. The missile has a two-stage solid propellant motor system, with a maximum range of 40 km. The second stage has lateral thrust motors to improve manoeuvrability in the terminal phase, similar to the US PAC-3 design. It can intercept targets from 5 m up to 20 km altitude. The 9M96/2 missile has a length of 5.65 m, a body diameter of 0.24 m, and a launch weight of 420 kg. The two missiles share the same separating second stage, but have different boost motors. The 9M96/2 missile has a maximum range of 120 km, and can intercept targets from 5 m up to 30 km altitude. The 40N6 version
图片：
:D :D
http://www.janes.com/extracts/extract/jsws/jsws9067.html
It is now believed that the Russian S-400 Triumf (Chinese designator HQ-19) surface-to-air missile system was a joint development programme with China. The system uses the same sensors, battle management and launch vehicles as the Russian S-300 (SA-10/-20 'Grumble') and Chinese HQ-9/-15. The S-400 introduces three new missiles, the 9M96, 9M96/2 and the 40N6, which can be fitted in new canisters replacing all or some of the S-300 missile canisters on the TEL. It is believed that a new TEL vehicle has been developed specifically to carry the S-400 missiles, and that this is a wheeled vehicle carrying six to eight missiles. The 9M96 missile has a length of 4.75 m, a body diameter of 0.24 m, a launch weight of 333 kg, and a 24 kg HE warhead. Guidance is inertial with command updates and an active radar terminal seeker. The missile has a two-stage solid propellant motor system, with a maximum range of 40 km. The second stage has lateral thrust motors to improve manoeuvrability in the terminal phase, similar to the US PAC-3 design. It can intercept targets from 5 m up to 20 km altitude. The 9M96/2 missile has a length of 5.65 m, a body diameter of 0.24 m, and a launch weight of 420 kg. The two missiles share the same separating second stage, but have different boost motors. The 9M96/2 missile has a maximum range of 120 km, and can intercept targets from 5 m up to 30 km altitude. The 40N6 version
图片：
:D :DHQ-19 (S-400)：
http://www.janes.com/extracts/extract/jsws/jsws9067.html
It is now believed that the Russian S-400 Triumf (Chinese designator HQ-19) surface-to-air missile system was a joint development programme with China. The system uses the same sensors, battle management and launch vehicles as the Russian S-300 (SA-10/-20 'Grumble') and Chinese HQ-9/-15. The S-400 introduces three new missiles, the 9M96, 9M96/2 and the 40N6, which can be fitted in new canisters replacing all or some of the S-300 missile canisters on the TEL. It is believed that a new TEL vehicle has been developed specifically to carry the S-400 missiles, and that this is a wheeled vehicle carrying six to eight missiles. The 9M96 missile has a length of 4.75 m, a body diameter of 0.24 m, a launch weight of 333 kg, and a 24 kg HE warhead. Guidance is inertial with command updates and an active radar terminal seeker. The missile has a two-stage solid propellant motor system, with a maximum range of 40 km. The second stage has lateral thrust motors to improve manoeuvrability in the terminal phase, similar to the US PAC-3 design. It can intercept targets from 5 m up to 20 km altitude. The 9M96/2 missile has a length of 5.65 m, a body diameter of 0.24 m, and a launch weight of 420 kg. The two missiles share the same separating second stage, but have different boost motors. The 9M96/2 missile has a maximum range of 120 km, and can intercept targets from 5 m up to 30 km altitude. The 40N6 version
图片：
:D :D
全是叉叉！
sg3366 发表于 2009-5-24 09:35 
国外屏蔽网站。找个代理服务器就可以浏览了。比如点击：:D
http://thesurfhide.com/index.php ... NzcuanBn&hl=1ed
国外屏蔽网站。找个代理服务器就可以浏览了。比如点击：:D
http://thesurfhide.com/index.php ... NzcuanBn&hl=1ed
谁发个图上来？
看不到图了
应该不是吧！！
红旗-19我相信不是毛子的。
我X。。。人鬼大人，这是5P85TE2啊。。。。。。。。。不会吧，毛子疯了不成？{:3_80:}
俺幼儿园级别的英语告诉俺。。。这。。。这TM也太霹雳了嘛。。。。。。。再{:3_80:}一个。
痴痴的小木头 发表于 2009-5-24 11:35
巴嘎 揪着耳朵乖乖回水区报道克先...[:a16:]
巴嘎 揪着耳朵乖乖回水区报道克先...[:a16:]
痴痴的小木头 发表于 2009-5-24 11:35
5P85TE2是啥？是S400的其中一个部分？
5P85TE2是啥？是S400的其中一个部分？
6楼那个图据说是S300换了个发射车~
{:3_76:}只凭拖车说明不了什么吧,这可能是最新交付的那批S300PMU2吧
5P85TE2是啥？是S400的其中一个部分？
spiderman 发表于 2009-5-24 11:40
可以看这片文章http://forum.defence.org.cn/viewthread.php?tid=23494
5P85TE2是啥？是S400的其中一个部分？
spiderman 发表于 2009-5-24 11:40
可以看这片文章http://forum.defence.org.cn/viewthread.php?tid=23494
spiderman 发表于 2009-5-24 11:40
毛毛的新版载重底盘 400露面样车时候配用的底盘
不排除毛毛把旧版底盘生产线升级造新的 以后所有出厂产品全用新车拉
毛毛的新版载重底盘 400露面样车时候配用的底盘
不排除毛毛把旧版底盘生产线升级造新的 以后所有出厂产品全用新车拉
rayghost 发表于 2009-5-24 11:50
我也觉得有可能是S300PMU2换了新的拖车。。。
我也觉得有可能是S300PMU2换了新的拖车。。。
车不等于蛋吧
车等于蛋么？个人觉得有可能是新一批次的S300PMU2，感觉不太可能会引进S400，一方面要地防空现在已经足够使用——我们周边除了美俄，装备弹道导弹的不多啊；另一方面TG发展的方向可能更近似于MD。
400你也要拆开看
改进在弹和雷达 都是分步进行
有点像阵风的F1 F2 F3形态改进
目前叫嚣很猛的400公里级别的弹靶场还没消息
要用
一阶段的400实际上用的PUM2 3外卖展示的配弹
原版300不也是从90射程的旧弹一步一步走过来的
改进在弹和雷达 都是分步进行
有点像阵风的F1 F2 F3形态改进
目前叫嚣很猛的400公里级别的弹靶场还没消息
要用
一阶段的400实际上用的PUM2 3外卖展示的配弹
原版300不也是从90射程的旧弹一步一步走过来的
车就和400一样，弹是不是就搞不清鸟
好早的图了.FY 08年就因为这个讨论过.大多数都认为是S300PUM2
It is now believed that the Russian S-400 Triumf (Chinese designator HQ-19) surface-to-air missile system was a joint development programme with China.
这句话不是盖的。:D
这句话不是盖的。:D
就是说S-400不是毛子单独搞的。原本就是我朝与俄罗斯联合出品。:D
当然是“根据”简氏。:D
现在确信俄罗斯 S400 凯旋（中国代号HQ19）地对空导弹系统是一项和中国共同的发展方案
去年找40N6的相关资料，看到这个网页，只发现最后是半句话没写完，应该扣网页编辑工资。
去年找40N6的相关资料，看到这个网页，只发现最后是半句话没写完，应该扣网页编辑工资。
再看看蛋蛋是啥货色 :D:D
http://proxyforall.com/proxysite ... NTIuanBn&hl=1ed
http://proxyforall.com/proxysite ... NTIuanBn&hl=1ed
打不开 人鬼先生
这就是中国进口的С-300ЛМУ2，所配的5Л85ТЕ2运输起竖发射车用了БАЗ-64022拖头
风卷云 发表于 2009-5-24 12:36
我这儿没问题啊。
上面的bombers先生再做一次好人吧。
我这儿没问题啊。
上面的bombers先生再做一次好人吧。
单看拖车也看不出来什么，如果有雷达就好识别了。
S-400 IZ Operational :
S-400 air-defence system operational
The Russian Federation Air Force (RFAF) has confirmed that two S-400 (Triumph) low- to high-altitude air-defence systems are in service with line units but that an extension of the re-arming effort depends on funding.
This information confirms a statement by Lieutenant General Aytech Bizhev, Deputy Commander-in-Chief (CinC) for the Commonwealth of Independent States Unified Air-Defence, that two S-400 systems are deployed with the air force for field testing and that these will be deployed fully in 2005.
The RFAF CinC General Vladimir Mikhaylov said on 11 December that the air-defence priority is to upgrade existing equipment and further develop the new S-400 for air defence and non-strategic missile defence.
Plans to re-arm the air force surface-to-air missile (SAM) units with the S-400 remain highly dependent on the availability of funds, and the manufacturing capacities of the industry, according to RFAF officials,.
Colonel General Boris Cheltsov, RFAF chief of staff, said the S-400 would achieve full operational readiness in 2005 after receiving a number of upgrades. Gen Bizhev also confirmed that the upgrades would allow the S-400 and the A-135M to share target data information.
Together with upgraded variants of the in-service SAM systems, the S-400 is part of an effort to "solve the issues of non-strategic missile defence". Gen Cheltsov, who headed the air force commission that supervised S-400 fire trials, said the commission has recommended to the Russian Ministry of Defence (MoD) that it accepts the S-400 in service "in a variant with a standard missile". Earlier it had been recommended that the S-400 enter trial service with missiles already used by the S-300 series.
Gen Bizhev said the S-400 would initially be located to protect Moscow, St Petersburg and the Urals industrial region, as well as border stretches "where missile attacks can be expected". He also said the S-400 could destroy cruise missiles and aircraft at a range of 250 km and at a range of heights from several dozen metres to the stratosphere.
The S-400, when operational with the new long-range missile (40N6), is claimed to have a range of 400 km and it is believed to have passed firing tests with all missile types.
The existing S-400s are currently undergoing capability enhancements for interoperability with the space forces assets.
The Russian armed forces say that the S-400 can potentially be used against strategic ballistic missiles after separation of warheads. In that role the S-400s will be co-operating with the A-135 anti-missile system in service with the Russian Space Forces. Provision is made for the S-400s to receive targeting information on approaching space threats from the Russian Space Forces in an automatic mode.
The S-400/A-135 will be the first block of the Air and Space Defence (ASD) system, a future structure concept recently formulated by the Russian defence ministry. The latter said that the MoD has recently approved the ASD concept and it is currently being improved for final validation by the Russian president.
Among other things, the ASD calls for a unitary radar field over Russia, similar to that which the Soviet Union had, but "on a new quality level". To achieve this, a united air traffic control/air-defence radar field will be created, combining the means of civil and military structures. Almaz-Antei (Air Defence Concern or Kontsern PVO) has been selected to lead the effort. Almaz-Antei will act as systems integrator and also supplier of major elements such as phased-array radar systems and 'identification friend or foe' interrogators. S-400 WILL Track Stealth Targets az well: S-400 surveillance radar will track stealth targets
Miroslav Gyürösi
Russia displayed the 96L6 surveillance radar for the S-400 missile system at the MAKS 2001 defence exhibition at Zhukovsky near Moscow, writes Miroslav Gyürösi. It operates in C-band, and the manufacturers say it can detect and track aircraft and cruise missiles which use stealth technology.
Work on the 96L6 began in the second half of the 1980s, when Boris Vasilyevics Bunkin, the general designer of CKB Almaz defined the requirements for a surveillance radar to form part of the new S-400 missile system. The design of the new radar was assigned to the Lira design bureau, which is a part of LEMZ - the Lianozovskiz Elektromekhanicseskij Zavod (Lianozovo Elektromechanical Factory). Lira and LEMZ are part of the financial-industrial group Oboronitelniye Sistemi (Defence Systems).
During the development and trials stage OKR (Opitno-Konstruktorskaya Rabota) of the programme, the new radar was designated VVO (Vsevisotniy Obnaruzhitel = detector for all altitudes).
The requirements for the VVO were very rigorous. The team headed by the late main designer Yuriy Fyodorovics Lisin based its design on research by Professor VI Vinokurov into the detection of difficult signals.
Another organisation involved with the development programme was the scientific research experimental establishment (Naucsno-Issledovatelskaya Eksperimentalnaya Rabota) Slozhnost (Complexity), whose general designers are BV Bunkin and Yuriy Aleksandrovics Kuznecov.
An experimental radar was built and tested in a series of trials against Yak-52 training aircraft. Specialists from other Russian radar establishments such as LETI, NII-2 MO, NII-3 MO, UPI, CNIIRES and VNIIRT participated in the trials, and the resulting data influenced the future development of radar technology in what was then the Soviet Union.
In 1988, representatives of the main developing organisation and the customer signed agreement giving the go-ahead for wideband radar technology, based on this earlier research to be used in the VVO programme. As a result of theoretical and experimental research, a database of difficult signals was developed, along with signal processing hardware with a speed of 10 billion operations per second, plus other components.
In 1991, the Lira design bureau built a prototype of the VVO radar. This started operation in early 1992, and in April of that year was demonstrated against low-altitude targets. Later that year systems were delivered for trials at the training centre of NII-2, the scientific research institute of the Russian air-defence forces. The system was displayed in model form at the MAKS 97 defence exhibition.
When the system enters service it will replace the 5N66M and 76N6 (NVO/NVO-M) radars currently used for the detection of low-flying targets. (The 76N6 is known to NATO as 'Clam Shell'.) Both had been developed in the early 1970s by the design bureau of the LEMZ factory. Later the 96L6 will replace the 19Zh6/35D6/36D6 family (ST-68U/-68UM) of all-round surveillance radars, which were developed and produced in Ukraine by NPO Iskra.
The role of the 96L6 is the detection of air targets and measuring of their azimuth, elevation and range. It can be used with the S-300PMU surface-to-air (SAM) system, can autonomously assign targets for the 90Zh6E, 90Zh6E1 and 90Zh6E2 (S-300PMU-1 and later) air-defence missile complexes, and can be connected with the Baykal-1E and Senezh-M1E automated command and control systems or the radiotechnical forces' Osnova-1E and Polye-E command posts.
It can pass information about a wide spectrum of the aerial targets, including aircraft, helicopters, UAVs and missiles, to the 30N6E, 30N6E1, 30N6E2 ('Flap Lid') series of tracking and missile guidance radars.
The 96L6 is very effective against low flying targets and against targets in the medium and high altitudes. It maintains its performance in the presence of heavy jamming, and has a very low false-alarm rate.
Targets can be tracked at elevations from 60º down to 0º, but a minimum of -3º is available as an option. The antenna uses several beams when scanning in elevation. For detection of very low flying targets, or if the radar is deployed in a wooded area, the antenna can be mounted on a 966AA14 elevated tower. The latter consists of a 40V6M tower mounted on a MAZ-537G (74106) truck.
There are two versions of the 96L6 - one which is installed on a single vehicle, and another which uses two vehicles.
The single-vehicle variant consists of:
• a 966AA01 antenna array;
• a 966FF03 shelter which houses the receiving, transmitting and information-processing subsystems, an operator console, communication and IFF systems and a ZIP-O repair set;
• a TM966 vehicle based on a Type 7930 Astrolog wheeled chassis with a SEP-2L generator and power-distribution system; and
• a set of cables.
The two-vehicle version consists of:
• a truck and trailer-mounted 966AA00 antenna set incorporating the 966AA01 antenna, an SES-75, SES-75M or equivalent model of electrical generator and power-distribution system, plus cables; and
• a truck and trailer-mounted 966FF00 installation incorporating the 966FF03 shelter and SES-75/-75M electrical system.
The two vehicles can be deployed up to 100m apart.
Operating frequency C-band (4-6GHz)
Range 5-300km
Maximum target elevation up to 60º
Maximum number of tracks up to 100 targets
Time from target detection to availability of target data:
- For elevations under 1.5º 12s
- For elevations over 1.5º 21s
Maximum number of the false target co-ordinates in 30min no more than 3-5
Crew 3
All-round search performance
Azimuth 360º
Elevation 0-20º (-3º if required)
Doppler speed range ±30 to ±1,200m/s
Information update rate:
- in the low zone (0-1.5º) 6s
- in the upper zone (1.5-20º) 12s
Sector search
Azimuth up to 120º
Elevation 0-60º (-3º if required)
Doppler speed range ±50 to ±2,800m/s
Time taken: sector search up to 8s
Time taken: lower sector search 5.5s
Time taken: full search cycle 13.5s
Low-altitude target search
Azimuth 360º
Elevation 0-1.5º
Doppler speed range ±30 to ±1,200m/s
Search time 6s
Deployment time from the move 5min (single-vehicle) 30min (two-vehicle)
Time needed to install antenna on the tower 120min
Activation time when in combat position no more than 3 min
Activation time when alerted no more than 40s
Continuous operating time no limits
Operating environment
Temperature ±50ºC
Dust up to 2.5g/m_
Wind up to 30m/s
Resistance to being over-turned by wind up to 50m/s
Operating altitude up to 3,000m
Service life before overhaul 10 years
Operating hours before overhaul 12,000h
Total service life 20+ years
Total operating hours 25,000-30,000h
S-400 IZ Operational :
S-400 air-defence system operational
The Russian Federation Air Force (RFAF) has confirmed that two S-400 (Triumph) low- to high-altitude air-defence systems are in service with line units but that an extension of the re-arming effort depends on funding.
This information confirms a statement by Lieutenant General Aytech Bizhev, Deputy Commander-in-Chief (CinC) for the Commonwealth of Independent States Unified Air-Defence, that two S-400 systems are deployed with the air force for field testing and that these will be deployed fully in 2005.
The RFAF CinC General Vladimir Mikhaylov said on 11 December that the air-defence priority is to upgrade existing equipment and further develop the new S-400 for air defence and non-strategic missile defence.
Plans to re-arm the air force surface-to-air missile (SAM) units with the S-400 remain highly dependent on the availability of funds, and the manufacturing capacities of the industry, according to RFAF officials,.
Colonel General Boris Cheltsov, RFAF chief of staff, said the S-400 would achieve full operational readiness in 2005 after receiving a number of upgrades. Gen Bizhev also confirmed that the upgrades would allow the S-400 and the A-135M to share target data information.
Together with upgraded variants of the in-service SAM systems, the S-400 is part of an effort to "solve the issues of non-strategic missile defence". Gen Cheltsov, who headed the air force commission that supervised S-400 fire trials, said the commission has recommended to the Russian Ministry of Defence (MoD) that it accepts the S-400 in service "in a variant with a standard missile". Earlier it had been recommended that the S-400 enter trial service with missiles already used by the S-300 series.
Gen Bizhev said the S-400 would initially be located to protect Moscow, St Petersburg and the Urals industrial region, as well as border stretches "where missile attacks can be expected". He also said the S-400 could destroy cruise missiles and aircraft at a range of 250 km and at a range of heights from several dozen metres to the stratosphere.
The S-400, when operational with the new long-range missile (40N6), is claimed to have a range of 400 km and it is believed to have passed firing tests with all missile types.
The existing S-400s are currently undergoing capability enhancements for interoperability with the space forces assets.
The Russian armed forces say that the S-400 can potentially be used against strategic ballistic missiles after separation of warheads. In that role the S-400s will be co-operating with the A-135 anti-missile system in service with the Russian Space Forces. Provision is made for the S-400s to receive targeting information on approaching space threats from the Russian Space Forces in an automatic mode.
The S-400/A-135 will be the first block of the Air and Space Defence (ASD) system, a future structure concept recently formulated by the Russian defence ministry. The latter said that the MoD has recently approved the ASD concept and it is currently being improved for final validation by the Russian president.
Among other things, the ASD calls for a unitary radar field over Russia, similar to that which the Soviet Union had, but "on a new quality level". To achieve this, a united air traffic control/air-defence radar field will be created, combining the means of civil and military structures. Almaz-Antei (Air Defence Concern or Kontsern PVO) has been selected to lead the effort. Almaz-Antei will act as systems integrator and also supplier of major elements such as phased-array radar systems and 'identification friend or foe' interrogators. S-400 WILL Track Stealth Targets az well: S-400 surveillance radar will track stealth targets
Miroslav Gyürösi
Russia displayed the 96L6 surveillance radar for the S-400 missile system at the MAKS 2001 defence exhibition at Zhukovsky near Moscow, writes Miroslav Gyürösi. It operates in C-band, and the manufacturers say it can detect and track aircraft and cruise missiles which use stealth technology.
Work on the 96L6 began in the second half of the 1980s, when Boris Vasilyevics Bunkin, the general designer of CKB Almaz defined the requirements for a surveillance radar to form part of the new S-400 missile system. The design of the new radar was assigned to the Lira design bureau, which is a part of LEMZ - the Lianozovskiz Elektromekhanicseskij Zavod (Lianozovo Elektromechanical Factory). Lira and LEMZ are part of the financial-industrial group Oboronitelniye Sistemi (Defence Systems).
During the development and trials stage OKR (Opitno-Konstruktorskaya Rabota) of the programme, the new radar was designated VVO (Vsevisotniy Obnaruzhitel = detector for all altitudes).
The requirements for the VVO were very rigorous. The team headed by the late main designer Yuriy Fyodorovics Lisin based its design on research by Professor VI Vinokurov into the detection of difficult signals.
Another organisation involved with the development programme was the scientific research experimental establishment (Naucsno-Issledovatelskaya Eksperimentalnaya Rabota) Slozhnost (Complexity), whose general designers are BV Bunkin and Yuriy Aleksandrovics Kuznecov.
An experimental radar was built and tested in a series of trials against Yak-52 training aircraft. Specialists from other Russian radar establishments such as LETI, NII-2 MO, NII-3 MO, UPI, CNIIRES and VNIIRT participated in the trials, and the resulting data influenced the future development of radar technology in what was then the Soviet Union.
In 1988, representatives of the main developing organisation and the customer signed agreement giving the go-ahead for wideband radar technology, based on this earlier research to be used in the VVO programme. As a result of theoretical and experimental research, a database of difficult signals was developed, along with signal processing hardware with a speed of 10 billion operations per second, plus other components.
In 1991, the Lira design bureau built a prototype of the VVO radar. This started operation in early 1992, and in April of that year was demonstrated against low-altitude targets. Later that year systems were delivered for trials at the training centre of NII-2, the scientific research institute of the Russian air-defence forces. The system was displayed in model form at the MAKS 97 defence exhibition.
When the system enters service it will replace the 5N66M and 76N6 (NVO/NVO-M) radars currently used for the detection of low-flying targets. (The 76N6 is known to NATO as 'Clam Shell'.) Both had been developed in the early 1970s by the design bureau of the LEMZ factory. Later the 96L6 will replace the 19Zh6/35D6/36D6 family (ST-68U/-68UM) of all-round surveillance radars, which were developed and produced in Ukraine by NPO Iskra.
The role of the 96L6 is the detection of air targets and measuring of their azimuth, elevation and range. It can be used with the S-300PMU surface-to-air (SAM) system, can autonomously assign targets for the 90Zh6E, 90Zh6E1 and 90Zh6E2 (S-300PMU-1 and later) air-defence missile complexes, and can be connected with the Baykal-1E and Senezh-M1E automated command and control systems or the radiotechnical forces' Osnova-1E and Polye-E command posts.
It can pass information about a wide spectrum of the aerial targets, including aircraft, helicopters, UAVs and missiles, to the 30N6E, 30N6E1, 30N6E2 ('Flap Lid') series of tracking and missile guidance radars.
The 96L6 is very effective against low flying targets and against targets in the medium and high altitudes. It maintains its performance in the presence of heavy jamming, and has a very low false-alarm rate.
Targets can be tracked at elevations from 60º down to 0º, but a minimum of -3º is available as an option. The antenna uses several beams when scanning in elevation. For detection of very low flying targets, or if the radar is deployed in a wooded area, the antenna can be mounted on a 966AA14 elevated tower. The latter consists of a 40V6M tower mounted on a MAZ-537G (74106) truck.
There are two versions of the 96L6 - one which is installed on a single vehicle, and another which uses two vehicles.
The single-vehicle variant consists of:
• a 966AA01 antenna array;
• a 966FF03 shelter which houses the receiving, transmitting and information-processing subsystems, an operator console, communication and IFF systems and a ZIP-O repair set;
• a TM966 vehicle based on a Type 7930 Astrolog wheeled chassis with a SEP-2L generator and power-distribution system; and
• a set of cables.
The two-vehicle version consists of:
• a truck and trailer-mounted 966AA00 antenna set incorporating the 966AA01 antenna, an SES-75, SES-75M or equivalent model of electrical generator and power-distribution system, plus cables; and
• a truck and trailer-mounted 966FF00 installation incorporating the 966FF03 shelter and SES-75/-75M electrical system.
The two vehicles can be deployed up to 100m apart.
Operating frequency C-band (4-6GHz)
Range 5-300km
Maximum target elevation up to 60º
Maximum number of tracks up to 100 targets
Time from target detection to availability of target data:
- For elevations under 1.5º 12s
- For elevations over 1.5º 21s
Maximum number of the false target co-ordinates in 30min no more than 3-5
Crew 3
All-round search performance
Azimuth 360º
Elevation 0-20º (-3º if required)
Doppler speed range ±30 to ±1,200m/s
Information update rate:
- in the low zone (0-1.5º) 6s
- in the upper zone (1.5-20º) 12s
Sector search
Azimuth up to 120º
Elevation 0-60º (-3º if required)
Doppler speed range ±50 to ±2,800m/s
Time taken: sector search up to 8s
Time taken: lower sector search 5.5s
Time taken: full search cycle 13.5s
Low-altitude target search
Azimuth 360º
Elevation 0-1.5º
Doppler speed range ±30 to ±1,200m/s
Search time 6s
Deployment time from the move 5min (single-vehicle) 30min (two-vehicle)
Time needed to install antenna on the tower 120min
Activation time when in combat position no more than 3 min
Activation time when alerted no more than 40s
Continuous operating time no limits
Operating environment
Temperature ±50ºC
Dust up to 2.5g/m_
Wind up to 30m/s
Resistance to being over-turned by wind up to 50m/s
Operating altitude up to 3,000m
Service life before overhaul 10 years
Operating hours before overhaul 12,000h
Total service life 20+ years
Total operating hours 25,000-30,000h
:D :D
34# 既非人又非鬼
神啊 ！
莫非是运矿的敞口散货车皮？
神啊 ！
莫非是运矿的敞口散货车皮？
天啊，tg太他妈的邪恶了
煤斗装导弹，首见
既非人又非鬼 发表于 2009-5-24 13:03
老大，这个红头就可以看出来是400？
老大，这个红头就可以看出来是400？
S400这个大神棍，忽悠体系不如我之体系忽悠
话说某某文曾言之某空间动能拦截器下有红旗XXX，如果结合各要地防空武器……恩，很好很强大的山寨MD体系
话说某某文曾言之某空间动能拦截器下有红旗XXX，如果结合各要地防空武器……恩，很好很强大的山寨MD体系
http://bbs.wefong.com/archiver/?tid-1882819.html
:)XD 2008-10-25 02:40 PM
1. 據報導中國已訂購5億美元的S-400
2. S-400於2007年8月6日服役
資料來源：維基百科英文版
yaklav 2008-10-26 06:50 AM
之前有傳言說中共是S-400系統開發出資者,不過即便此事是真,依照去年八月六日開始服役、而正式形成戰力則是要到年底,所以雖然開始量產,而且俄國為了在部分區域反制美國的反飛彈系統包圍網、因此態度頗為積極地推銷S-400,不過照普通武器系統的狀況來看,至少俄國的一線防空部隊要換裝的差不多了才能開始大量外銷,所以即便已經簽約訂貨,也難以在最近兩三年到貨並進入服役。
:)XD 2008-10-25 02:40 PM
1. 據報導中國已訂購5億美元的S-400
2. S-400於2007年8月6日服役
資料來源：維基百科英文版
yaklav 2008-10-26 06:50 AM
之前有傳言說中共是S-400系統開發出資者,不過即便此事是真,依照去年八月六日開始服役、而正式形成戰力則是要到年底,所以雖然開始量產,而且俄國為了在部分區域反制美國的反飛彈系統包圍網、因此態度頗為積極地推銷S-400,不過照普通武器系統的狀況來看,至少俄國的一線防空部隊要換裝的差不多了才能開始大量外銷,所以即便已經簽約訂貨,也難以在最近兩三年到貨並進入服役。