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Last Updated: Mon Jan 27 11:18:09 UTC 2014







S-300P/S-400/S-500 Air Defence System Vehicles


Technical Report APA-TR-2008-0601-A


by Dr Carlo Kopp, AFAIAA, SMIEEE, PEng
June 2008
Updated February, 2010
Updated May, June, 2011
Updated April, 2012
Text © 2008-2012 Carlo Kopp
 





Slovakian Air Force S-300PMU / SA-10B 30N6-1 Flap Lid B and 83P6 Fire Unit comprising one 5P85SE TEL and a pair of 5P85DE TELs at Piestany in 2009 (© 2009 Miroslav Gyűrösi).



Introduction


Since its introduction over three decades ago the S-300P family of SAM systems has become one of the most widely used designs in its class, globally, and currently forms the backbone of both Russia's and China's extensive national IADS. Almost four decades of technological evolution has seen considerable diversity in variants deployed, reflected in a wide range of different radars, command posts, Transporter Erector Launchers, and other support vehicles employed.

A range of different military truck chassis have been employed to host or tow S-300P battery components since the first S-300PT systems were built. The choices in these vehicles reflect repeatedly period priorities, be they in offroad mobility, procurement costs, production availability, or most recently, sources of supply with the breakdown in relations between Russia and the Ukraine.

From a technical intelligence perspective, this diversity in vehicles is important. Some variants can only be visually differentiated by the vehicle types employed, whether the imagery is close-in or overhead. The different vehicles also provide differing levels of offroad mobility, contraining deployment choices in off-base hide, shoot and scoot operations.

The earliest S-300PT systems were mobile, but did not qualify as hide, shoot, and scoot systems. Battery components were mounted on trailers or semi-trailers, towed by the Russian Ural 375 or Ukrainian KrAZ-255 6 x 6 trucks. Only the massive 40V6M/MD mast system was towed by the MAZ-537 series heavy tractor, widely used for ballistic missile and tank transporter towing.

Significant changes arose with the introduction of the self-propelled S-300PS / SA-10B, and its export derivative, the very similar S-300PMU (often labelled an SA-10C). This variant introduced the MAZ-7910 chassis, based in the MAZ-543M Uragan which was widely used as a ballistic missile TEL. Often considered to provide similar offroad mobility to tracked armour, the MAZ vehicles were a very robust solution to the mobility problem. The 5N63S Flap Lid B  engagement radar, the early 5N64 Big Bird battle management radar, and the 5P85D/S TELs all employed this vehicle. Variants of the MAZ-7910 chassis have remained on offer for all subtypes including the S-300PMU-2 Favorit / SA-20B.

The next significant variant to deploy was the S-300PM, a deep upgrade of the radar, systems and missile round design. The S-300PM formed the basis of the S-300PMU1 and S-300PMU2 Favorit export variants. While the S-300PM was supplied with the MAZ-7910 based  self-propelled TEL design, this variant also saw the introduction of a towed TEL, the 5P85T, and its export derivative 5P85TE/TE1/TE2 variants. Until recently, the 5P85T series TELs were supplied with Ukrainian built KrAZ-260B tow tractors, supplanted now by Russian built BAZ-69022 series tractors, also employed with early production S-400 Triumf / SA-21 systems.

Russian sources have claimed that development is proceeding on the 5P90 series TEL, but no details have been disclosed to date.


Future Voshchina Series S-400 Battery Vehicles



BAZ-64022 towing a 5P85TE2 TEL (© 2011, Vitaliy Kuzmin).


Long term planning by Russia's PVO is to replace all S-300P/S-400 family SAM system vehicles with various derivatives of the BZKT BAZ-6402/6909 Voshchina 1 and 2 family of vehicles, supplanting imported Belarus MZKT MAZ-7900 series vehicles used as TELs, for carrying radar systems, towing radars, and the widely used Ukrainian KrAZ-260 and Belarus MAZ-537 tow tractors.

The 92N6 Grave Stone and 96L6 will be carried on the 8 x 8 BAZ-69096 chassis.

A new BAZ-6403 derivative tractor is to be used to tow the 91N6 Big Bird battle management radar, and 40VM series mobile mast systems, supplanting the 1990s MZKT-7930 and 1960s MAZ-537 8 x 8 tractors.

TEL options for the S-400 and planned S-400M include the baseline 5P85TE2 semitrailer, towed by a 6 x 6 BAZ-64022, the improved  5P90S self-propelled TEL, believed to be based on the BAZ-6909 series and intended to carry a heavier missile payload than the legacy MAZ-79100 series TELs, and a new heavyweight towed TEL to be designated the 5P90TMU.

Both the BAZ-6402 and BAZ-6403 are cited as tow tractors for the 40V6M and 40V6MD masts, and derivative 40V6M-R and 40V6M-R-0 masts. The BAZ-6403 is a shortened chassis 8 x 8 tow tractor built for heavier loads than the BAZ-6402.

Other cited applications for the 6 x 6 BAZ-6402 include towing the 5T58 missile transporter semi-trailer, and the BAZ-6403 include towing the 15G95M and 15G96M refuelling equipment, and a range of ChMZAP series tank and vehicle transporter semi-trailers.

The 8 x 8 BAZ-6909 is also intended as a host vehicle for the 9T243M transloader/transporter, and was also used for the prototypes of the advanced NNIIRT 55Zh6M Nebo M  VHF-Band  and L-Band Counter-VLO radar.

The production 64L6E Gamma-S1E radar system is hosted on the 6 x 6 BAZ-69092 vehicle, which is also being adapted as the host vehicle for the 22T6/22T6E missile transloader for the S-300P/S-400 series. The 8 x 8 BAZ-69092-021 has been adapted to tow the 5I57 deployable diesel electric generator / power converter system used for static S-300P/S-400 sites.

The 8 x 8 BAZ-69096 chassis is also intended for future use in the 96K6 Pantsir S1 / SA-22 SPAAGM, which will co-deploy with S-400 batteries to provide terminal Counter-PGM capability against anti-radiation missiles and guided bombs. It also the designated host vehicle for the new 50R6 Vityaz point defence SAM system, armed with the Fakel 9M96E/E2 missiles, its 50N6 multimode engagement radar, and 50K6 command post.

A 10 x 10 derivative of the BAZ-6909 series is also the intended platform for rehosting the 3K81MK/S-300VMK/SA-23 PVO-SV SAM system, but it is not clear this system will enter production. It may however appear as a block upgrade to extant SA-12 Gladiator/Giant systems if these remain in service longer.

The Voshchina series vehicles are better hardened than their predecessors, and this includes bullet-proof windows on vehicles supplied to the Russian armed services. Powerplants vary across subtypes, and include the YaMZ-849.10 turbocharged 500 SHP diesel, and the TMZ-8424.10-033 turbocharged 470 SHP diesel. The basic crew cabin has three side by side seats, although some subtypes have only two seats to make space for mission equipment.

While the cited reason for replacing Belarus and Ukrainian built vehicles with Russian built vehicles is to preclude a repeat of the post Orange Revolution breakdown of imported component supplies, there may be more pragmatic considerations in play. A common Voshchina series chassis provides not only logistical commonality and thus lower operating costs, but also permits common training of drivers and mechanics, and importantly, all battery components have identical cross country capability and road speed in high mobility operations, including the C-PGM battery.

All Voshchina series vehicles are designed to be compatible with the An-22 Cock, Il-76 Candid and An-124 Condor airlifters.


BAZ-6909 Voshchina I Variants
БАЗ-6909 «Вощина-1»




BAZ-6910 artillery tractor (© 2011, Vitaliy Kuzmin).



BAZ-6910 artillery tractor (© 2011, Vitaliy Kuzmin).



BAZ-6910 artillery tractor (© 2011, Vitaliy Kuzmin).



BAZ-6910 artillery tractor (© 2011, Vitaliy Kuzmin).



BAZ-6909 engineering vehicle (Russian Internet).



BAZ-69092 tractor (Russian Internet).

x

The BAZ-6403 is a dedicated tractor for semi-trailer payloads, such as tank transporters and fuel tankers. It is also intended to tow the 91N6 Big Bird radar and 40V6M series mobile mast systems (BZKT Factory Image).



Above, below: BAZ-6909 artillery tractor (Russian Internet).





BAZ-6910 cabin (© 2011, Vitaliy Kuzmin).



NNIIRT Nebo-M RLM-D L-band radar on BAZ-6909 vehicle, stowed (NNIIRT).



NNIIRT Nebo-M RLM-D L-band radar on BAZ-6909 vehicle, deployed (NNIIRT).



RLM-M component of the NNIIRT 55Zh6M Nebo M, based on the VHF band Nebo SVU. This is effectively a true "shoot and scoot" self-propelled derivative of the Nebo SVU demonstrator design, hosted on a BAZ-6909-022 high mobility chassis (NNIIRT).



Baseline Gamma S1/S1E on the BAZ-64022 chassis, the RLM-S will be a similar configuration (Said Aminov Vestnik-PVO).






NNIIRT Nebo M System Components
KU
Central track processing and fusion system with multiple operator consoles.
RLM-M
Self-propelled AESA radar based on VHF band Nebo SVU design
RLM-D
Self-propelled AESA radar based on L band Protivnik G design
RLM-S
Self-propelled AESA radar based on S/X band Gamma S1 design



Fully deployed 72V6 SPAAGM prototype on BAZ-6909 chassis. The primary design aim for this system was the interception of PGMs, especially the AGM-88 HARM and GBUs. It will co-deploy with S-400 batteries (Sergei Kuznetsov via Strizhi.ru).



BAZ-6909-015 (BZKT Factory Image).



BAZ-6909-015 (BZKT Factory Image).



BAZ-6909-015 (BZKT Factory Image).



BAZ-6909-019 (BZKT Factory Image).



BAZ-6909-019 (BZKT Factory Image).



BAZ-6909-022 (BZKT Factory Image).



BAZ-6909-022 (BZKT Factory Image).




BAZ-6909-022 (BZKT Factory Image).



BAZ-6403 8x8 Tractor (BZKT Factory Image).



BAZ-6403 8x8 Tractor (BZKT Factory Image).











S-300VMK in stowed configuration. The 9A82MK TELAR and 9A84MK, 9A85MK TELs are not depicted. Note the large elevating mast on the 9S457MK CP (Russian Internet - unknown author).



BAZ-69096 during trials (image © 2011 Michael Jerdev).

 Характеристики БАЗ-6909 БАЗ-69091 БАЗ-69096
Колёсная формула 8×8 10×8
Количество мест в кабине 4
Длина, мм 11300 12400 14250
Ширина, мм 2750
Высота, мм 3088
Дорожный просвет, мм 485
Радиус поворота, м 13,5 14,0 16,35
Снаряженная масса, т 18,2 17,5 19,9
Грузоподъемность, т 18,0 17,5 29,5
Масса буксируемого
прицепа/полуприцепа, т
15,0 -
Двигатель (тип) ЯМЗ-8424.10 (Д, V12)
Мощность двигателя, кВт/л.с. 294/400
Максимальная скорость, км/ч 80 70
Преодолеваемый подъем, град 30
Преодолеваемый брод, м 1,4
Запас хода по контрольному расходу топлива, км 1000 900
Source: Russkaya Sila, URI: http://legion.wplus.net/guide/army/tr/baz6909.shtml

БАЗ-6403 Параметры
Наименование Значения

Колесная формула,

8х8.1

Нагрузка на седельно-сцепное устройство, тс

19,5

Снаряженная масса, т

17,7

Полная масса автопоезда, т, не более

65,0

Двигатель дизельный с турбонаддувом,

ЯМЗ-8424.10

Мощность двигателя, л. с.

425

Сцепление однодисковое диафрагменное,

ЯМЗ-184.10

Коробка передач, 9 передач вперед, 1 назад,

ЯМЗ-2393-03

Подвеска I и II осей,

независимая двухторсионная с амортизаторами на каждом колесе

Подвеска III и IV осей,

комбинированная независимая одноторсионная для нижних рычагов и балансирная для верхних

Шины с регулируемым давлением, радиальные (1350х550-533Р),

ИД-370

Минимальный радиус поворота, м

14,0

Максимальная скорость, км/ч

60

Запас хода по контрольному расходу топлива, км

1000

Габаритные размеры

Длина, мм

9595

Ширина, мм

2750

Высота, мм

2850

Двигатель

Марка двигателя,

ЯМЗ-8424.10

Мощность, л.с.

425

Source: BZKT http://bzkt.ru/production.html?section=1&position=21


S-300P/S-400/S-500 Variant TEL Design

There are three generations of TEL design employed with variants of the S-300P system. Many share vehicle chassis, launcher hardware, and/or mission electronics.

DIA
Soviet/Russian Designation
SP TEL Variants
Towed TEL Variants
Notes
SA-10A
S-300PT -
5P85-1
Soviet
SA-10B
S-300PS 5P85S + 5P85D -
Soviet
SA-10B[C]
S-300PMU 5P85SU + 5P85DU -
Export PS
SA-20A
S-300PM 5P85SM/SE 5P85T Soviet
SA-20A
S-300PMU1 5P85SM/SE 5P85TE Export PM
SA-20B
S-300PMU2 Favorit
5P85SM/SE 5P85TE
5P85TE2
Export
SA-21
S-400 Triumf
5P90S 5P85T2/TE2 Russian
Export
SA-X-NN
S-500
5P77
-
Russian
Table 1 S-300P Family SAM System TEL Configurations

The earliest towed 5P85/5P85-1 TELs were a stopgap design, produced to permit earliest possible deployment of the S-300PT system. This rather ungainly design, in which the tow booms were splayed out as supports, is easily distinguished visually, and carries the missile launch tubes oriented with the exhaust toward the tow tractor. It introduced the characteristic hydraulically elevated boom mounting the four missile launch tubes in a unique symmetrical trapezoidal arrangement.


S-300PT 5P85-1 TEL (Vestnik PVO)

The cold launch missile technology, whereby the round was ejected vertically from the tube prior to main engine ignition, was developed initially for ballistic missile launches from silos. It was attractive for a SAM system as the TEL did not need to be protected heavily against high temperature exhaust efflux, a problem with earlier designs. The sealed "wooden round" launch tube doubled up as a transport container, simplifying the whole logisitical chain for reloads, an enormous advancement over the rail launched liquid fuelled S-75 and S-200 systems the S-300P was to replace, both of which required fuelling and partial missile re-assembly in the field. Missile reloads were carried by a 5T58 semi-trailer, usually towed by a KrAZ or Ural 6 x 6 tractor. Transloading was performed initially using a crane, and later using a specialised hydraulic 5T99 transloader vehicle.

The TEL boom design comprises two main sections. The load bearing lower section is  formed by a pair of rigid structural boxes with internal spacing members. It pivots at one end of the TEL chassis, and is elevated or stowed using a hydraulic boom. Two adaptors are mounted to it, providing a conformal load relief and attachment for the four launch tubes.

The top of the boom mounts a characteristic latticework frame which carries the four  U-shaped missile control and status umbilical cables and connectors. When a launch tube is attached, the connectors are mated to the tube to permit the transfer of missile and tube diagnostic, status and control commands. This arrangement has been retained, with variations, in all S-300P variants, including the S-400.



Partly loaded and stowed S-300PMU 5P85SE TEL of the Slovakian Air Force (upper), and empty TEL (lower). Note the umbilicals for the missile launch tube containers (© Miroslav Gyűrösi).





Deployed S-300PMU 5P85DE TEL of the Slovakian Air Force. The canvas shroud over the utility area is almost identical in shape to the F3S cabin (© Miroslav Gyűrösi).


Deployed S-300PMU 5P85SE TEL of the Slovakian Air Force (via valka.cz).



Conformal attachments for launch tubes (via valka.cz).

The self-propelled 5P85S/D TELs introduced first in the S-300PS provided a much more flexible deployment scheme, but not without limitations.

The 5P85S with the characteristic large F3S accessory cabin and the supplementary 5P85D TEL, were both equipped with 5S18/19 series autonomous gas turbine electrical power generators,  to permit standalone operation without an external generator van.

A typical S-300PS/PMU battery 5P85SD TEL "komplex" would include one 5P85S/SU TEL, two 5P85D/DU TEL/Transloaders, all controlled by one self-propelled 5N63S Flap Lid B radar. The 5P85S was a "smart" TEL equipped with the control logic and datalink hardware for the whole 5P85SD TEL group, the 5P85D being a "dumb" TEL under the control of the 5P85S (the mnemonic is accidental).

The principal limitation of this scheme was that TEL arrangement forced pairing of two 5P85Ds with a single 5P85S which controlled the group. This limited deployment options and flexibility in hide, shoot and scoot operations. The dumb 5P85D/DU TELs needed to be sited several metres from the 5P85S/SU smart TEL, this being limited by cable length. The whole TEL group had to be sited within 100 metres of the 5N63S Flap Lid B engagement radar, due to the limited range of the radio datalink between the radar and smart TEL.

The S-300PM and S-300PMU1 export variant rectified this problem with the third generation of TELs, in which every TEL was smart and fully autonomous. Two distinct designs were introduced, sharing common hardware across different chassis. The 5P85SM and 5P85SE were smart self-propelled TELs on the MAZ chassis, with the distinctive bulky F3S cabin used with the 5P85S/SU replaced by much smaller electronics enclosures. This TEL has been offered, with electronics enhancements, for the S-300PMU2. The alternative was the cheaper road mobile 5P85T towed TEL, which has dominated deliveries in later variants. Both variants retain spools for umbilical cables, permitting cabled connections to the 30N6E series radar if desired. In additional, each TEL carries a main power converter and 60 metre power cable. All TEL functions, including elevating or stowing the launchers, are performed remotely over the radio datalink.

TEL Datalink Antennas







There are two different datalink antenna configurations employed with late model 5P85 family TELs. This is distinct from the common telescoping F-24 family datalink antenna/mast assembly employed across a range of Flap Lid, Tomb Stone and Grave Stone engagement radar variants. The most commonly used antenna design appears to be a variation on the parallel plate antenna theme, mounted on a simple tubular mast of around 2 metres in length (above). This design is intended to radiate horizontally, with a likely null in the direction of the launcher tubes. The low gain and limited elevation of the antenna will limit range severely.  A more elaborate antenna design, with a telescoping mast and four elements, also exists (left - Almaz-Antey image) but has not been observed on operational TELs, with the first example seen on the new 5P90S TEL. This design provides high mast elevation, and directional emission, requiring the antenna be pointed at the engagement radar.







S-300PMU / SA-10B[C] Grumble battery tie-in chart. Four 83P6 Fire Units, each comprising a 5P85SE TEL, and two 5P85DE TELs, must be located within 120 metres of the 30N6-1 Flap Lid B engagement radar, which contains the battery command post. The ST-68UM Tin Shield and 76N6 Clam Shell acquisition radars must be located within 250 metres and 500 metres, respectively, of the Flap Lid. Connectivity to a 5S99-M Senezh-M or 5N37/73N6 Baikal ADCP is via  landlines or a mobile microwave relay link, such as the telescopic mast equipped FL-95 microwave relay link on a ZiL-131 chassis (Slovakian AF vs Miroslav Gyűrösi).



Deployed 5P90S TEL with elevated long range datalink mast (image © 2011 Michael Jerdev).


Late model S-300P system TELs are highly automated, and will level automatically on hydraulic supports once initiated by the crew. This decouples the system stow/deploy time from operating crew proficiency, the task of the crew being simply to drive the TEL to an intended location, deploy it, and then stow it and relocate once required. The TEL is fully remotely controlled by the engagement radar over the radio datalink channel, and missiles are launched remotely.

Future developments in this TEL family are likely to involve not only newer vehicles, but also improvements in datalink/network technology, and progressively, the introduction of precision positioning capability in TEL, not unlike the Orientir system developed for the 30N6E2 Tomb Stone.


S-300P/S-400/S-500 Transporter Erector Launcher Vehicles


77P6 Self Propelled Transporter Erector Launcher



Systems: S-500

In development for the S-500 SAM/ABM system, the 77P6 is closest in appearance to the 9A82MK TEL for S-300VMK, including the use of the legacy 9A82/9A84 gantry and 9Ya238 Missile Launch Tube / Transport Container, used for the 9M82/9M82M / SA-12B/SA-23B Giant missile. Prominent differences from the 9A82MK/9A83MK are the accessory housings, which are considerably more compact, and an outrigger design common to the self-propelled S-400 9P90S TEL. The drawing shows no evidence of the CW illuminator/uplink antenna used with S-300V/VM TELARs, and does not include the NK Orientir precision navigation system, which may be an omission. The missile types carried were not disclosed as of June, 2011.


 
The 77P6 TEL is to be hosted on a variant of the 10 x 10 BAZ-69096 (images © 2011 Michael Jerdev).







5P90S/SE Self Propelled Transporter Erector Launcher

5P90TMU Towed Transporter Erector Launcher



Deployed 5P90S self-propelled TEL (All 5P90S images © 2011 Michael Jerdev).

Systems
: S-400

The 5P90 series are the new TEL designs for the S-400 Triumf / SA-21 SAM system. The improved  5P90S self-propelled TEL is hosted on the BAZ-6909-022 and intended to carry a heavier missile payload than the legacy MAZ-79100 series TELs.

Imagery of the 5P90S self-propelled TEL shows a new gantry design, a new elevating folding mast with a directional antenna, and a state-of-the-art NK Orientir precision navigation system, with an increased baseline for the satnav antennas, compared to the installation on the S-300PMU2 vehicles.

The new mast and datalink antenna has important implications, as this will permit TELs to operate at considerably greater distances from the engagement radar, compared to earlier S-300P family SAM systems. The directional antenna system will significantly reduce the susceptibility of the TELs to interception, and geolocation by passive RF sensors. This will make dispersed TELs stealthier, and thus more difficult to locate, jam and/or attack with lethal weapons.

The evolved NK Orientir navigation system will permit TELs to accurately geolocate, relative to the engagement radars, and facilitates the use of a narrow beam directional datalink.

The significance of the revised gantry design remains unstated, but may reflect increased launch weight in later missile variants.



Above, below: Stowed 5P90S during demonstration trials (image © 2011 Michael Jerdev).


(image © 2011 Michael Jerdev)



(image © 2011 Michael Jerdev)



(© 2011 Vitaliy V. Kuzmin)



(© 2011 Vitaliy V. Kuzmin)



(© 2011 Vitaliy V. Kuzmin)

 

(© 2011 Vitaliy V. Kuzmin)



Detail of 5P90S cabin, roof mounted navigation system antenna suite, and deployed datalink mast  (image © 2011 Michael Jerdev).



Detail of 5P90S hydraulically deployed datalink mast. Four antenna elements of yet to be disclosed gain are employed (image © 2011 Michael Jerdev).



Detail of 5P90S hydraulically deployed datalink mast in stowed position. The position of the  stowed antenna elements suggests the design is steerable in azimuth (image © 2011 Michael Jerdev).



Above, below: Detail of 5P90S gantry, deployed. The design appears structurally more robust than the 5P85 series gantries (image © 2011 Michael Jerdev).


5P90S/SE Self Propelled Transporter Erector Launcher Deploy/Stow Sequence
(All 5P90S images © 2011 Michael Jerdev; © 2011 Vitaliy V. Kuzmin)

Deployment and stowing of the 5P90S, and earlier 5P85 series  self propelled TELs, is substantially automated to permit 5 minute deploy and stow times for high mobility operations.

Once the TEL is positioned, the APU is started, and the outriggers deployed to stabilise the chassis. Levelling is performed by differential outrigger settings. Once stable and levelled, the gantry is hydraulically elevated into the vertical position. The datalink antenna mast can then be deployed. Following missile BIT the TEL can go online and accept launch commands from the Grave Stone engagement radar.

Following missile launch, or a directive to redeploy, the datalink antenna mast and gantry can be hydraulically stowed, and the outriggers retracted. At that point the TEL can redeploy to evade attack. It is likely that actual stow times are shorter than deploy times, as there is no need to perform TEL levelling.

Warsaw Pact and Soviet practice with the S-300PS/PMU/PM was to often drape camouflage nets over portions of the TEL, including the missile launch tube/containers. If these nets are radar and infrared opaque, identification and recognition of the TEL using SAR or FLIR may present genuine difficulties.



Once levelling is completed, the gantry is hydraulically elevated to vertical position (© 2011 Michael Jerdev).



(© 2011 Michael Jerdev)



(© 2011 Michael Jerdev)



5P90S TEL deploying antenna (© 2011 Vitaliy V. Kuzmin).




(© 2011 Michael Jerdev)



(© 2011 Michael Jerdev)



With the gantry and mast stowed, the outriggers can be retracted and the TEL can redeploy (© 2011 Michael Jerdev).


5P85TM/T2/TE2 Towed Transporter Erector Launcher



Systems: S-400; Late Production S-300PMU2

The new 5P85TM/T2/TE2 series TEL combines a variant of the legacy 5P85TE1 TEL semi-trailer with a new 6 x 6 BAZ-64022 tow tractor, the latter based on the Bryanskiy Avtomobilnyy Zavod (Брянский автомобильный завод) BAZ-69092 "Voshchina 1" series of military trucks. The BAZ-64022 is based on the BAZ-6402 artillery tractor.



BAZ-6402 Specifications

Наименование Значения

Колесная формула,

6х6.1

Нагрузка на седельно-сцепное устройство, тс

11,5

Снаряженная масса, т

16,0

Полная масса автопоезда, т, не более

45,8

Двигатель дизельный с турбонаддувом,

ЯМЗ-8424.10

Мощность двигателя, л. с.

470

Сцепление однодисковое диафрагменное,

ЯМЗ-184.10

Коробка передач, 9 передач вперед, 1 назад,

ЯМЗ-2394

Подвеска I оси,

независимая двухторсионная с амортизаторами на каждом колесе

Подвеска II и III осей,

комбинированная независимая одноторсионная для нижних рычагов и балансирная рессорная для верхних

Шины с регулируемым давлением, радиальные (1350х550-533Р),

ИД-370

Минимальный радиус поворота, м

13,0

Максимальная скорость, км/ч

70

Запас хода по контрольному расходу топлива, км

1000

Габаритные размеры

Длина, мм

9180

Ширина, мм

2750

Высота, мм

2850

Двигатель

Марка двигателя,

ЯМЗ-8424.10

Мощность, л.с.

470







The 5P85TE2 TEL towed by a 6 x 6 BAZ-64022 tractor is a distinctive feature of the S-400, making it readily identifiable in comparison with the KrAZ-260 towed 5P85TE variants used with the SA-20 Gargoyle (Almaz-Antey/Vestnik PVO).


Above, below: BAZ-64022 tractor (© 2011, Vitaliy Kuzmin).


MZKT-7930 Self Propelled Transporter Erector Launcher

Systems: S-400

An option listed at one stage by Almaz-Antey for the S-400 is an 8 x 8 TEL based on the MZKT-7930 chassis, almost certainly involving a transplant of the hydraulically elevated erector/launcher equipment from the S-400 5P85SE demonstrator TEL on to the newer chassis design. To date no images of this design have appeared. It would deliver similar cross country performance to the legacy 5P85SE TELs.


(MZKT drawing)

5P85T/TE Towed Transporter Erector Launcher



S-300PMU2 Favorit 5P85TE TEL Deployed (
© Miroslav Gyűrösi).

Systems: S-300PMU1/PMU2

The production 5P85TE TEL combines a variant of the 5P85TE TEL semi-trailer with the Ukrainian Kremenchugskiy AvtoZavod 6 x 6 KrAZ-260 tow tractor. The KrAZ-260 entered production in 1979 as an artillery tow tractor, with variants built for a range of military and civil applications. Typical variants are rated in the 9.5 to 10 tonne class. It was introduced to provide a much cheaper TEL compared to the MAZ-543 derived 5P85D/S series, sacrificing offroad mobility in the process, but improving road speed.

Грузоподъемность, (без лебедки) 9500 кг.

Снаряженная масса (без лебедки и дополнительного снаряжения) 11750 кг.
В том числе:
на переднюю ось 5740 кг.
на тележку 6010 кг.

Полная масса 21475 кг.
В том числе:
на переднюю ось 6320 кг.
на тележку 15155 кг.

Допустимая полная масса прицепа:
по всем видам дорог и местности 10000 кг.
по дорогам с твердым покрытием 30000 кг.

Макс. скорость автомобиля 80 км/ч.
То же, с прицепом полной массой 10000 кг 80 км/ч.
Время разгона атомобиля до 60 км/ч 40 с.
Выбег автомобиля с 50 км/ч 650 м.
Макс. преодолеваемый подъем автомобилем 58 %
То же, с прицепом полной массой 10000 кг 32 %
Тормозной путь автомобиля с 40 км/ 17,2 м.
То же, автопоезда 18,4 м.

Контрольный расход топлива автомобиля, л/100 км, при скорости 60 км/ч 38,5 л.
Глубина преодолеваемого брода с твердым дном при номинальном давлении воздуха в шинах 1,2 м.

Радиус поворота:
по внешнему колесу 13,0 м.
габаритный 13,5 м.
Двигатель.
Мод. ЯМЗ-238Л. дизель с турбонаддувом V-образный 8-цил., 130x140. 14,86 л, степень сжатия 1 5 , 2 , порядок работы 1-5-4-2-6-3-7-8, мощность 220 кВт (300 л.с.) при 2100 об/мин, крутящий момент 1079 Н-м (110 кгс-м) при 1500 об/мин. ТНДВ - 8-секционный,






5P85TE TELs towed by KrAZ-260 tractors.


5P85S/SM/SE/SE1/SE2 Self Propelled Transporter Erector Launcher

5P85S/SU and 5P85D/DU Self Propelled Transporter Erector Launcher


Systems: S-300PS (D/DU/S/SU); S-300PM/PMU1/PMU2 (SM/SE)

The 5P85SE variants delivered with early production examples of the S-300PMU2 Favorit / SA-20B SAM systems are the last production variants of the family of 8 x 8 self-propelled TELs introduced with the S-300PS system during the 1980s. These are all based on variants of the MAZ-7910 chassis, itself a derivative of the ByeloRussian MAZ-543/543M Uragan chassis series developed as the self propelled 9P117 TEL for the R-17/R-300 Elbrus / SS-1 Scud TBM. The MAZ-543 was soon dubbed Kashalot  (Sperm Whale) by its crews due to its sheer size compared to earlier Soviet wheeled vehicles. This vehicle has remained in production in various forms since the early 1960s, and has been adapted for the Smerch MRLS, a range of radar systems, and formed the basis for larger 12 x 12 ballistic missile TELs, cranes, oilfield trucks, artillery tow tractors, and semitrailer two tractors.



9P117 Kashalot TEL for the R-17/R-300 Elbrus / SS-1 Scud TBM using the MAZ-543 Uragan chassis (Czech Army).

The MAZ-7910 chassis first appeared with the S-300PS / SA-10B Grumble, the S standing for Samokhodniy (Self Propelled). The vehicle was used initially for the 5P85DU and 5P85SU TELs,  the 30N6 Flap Lid series of engagement radars, and the 54K6 and 73N6 Baikal command posts. The base vehicle was later adapted as the MAZ-74106 tow tractor for the 64N6 Big Bird acquisition radar. In one or another form the MAZ-7910 forms the basis for most highly mobile S-300P variant systems.

The first generation S-300PS TEL variants differed. The 5P85S was a fully autonomous or 'master' TEL, the 5P85D a 'slave' TEL, usually deployed in pairs with a single 5P85S. Later TEL variants such as the 5P85SE, 5P85SE1 and 5P85SE2 were all derived from the autonomous 5P85S series. The enclosed cabin used in the 5P85S/SU vanished in later variants of the 5P85SE.

MAZ-543 Uragan General Specifications
Parameter
Metric Magnitude [unit]
Imperial Magnitude [unit]
Length
11,245 [mm]
Width
3,050 [mm]
Height
2,945 [mm]
Wheelbase
7,700 [mm]
Turn Radius
13.5 [m]

Ground clearance 400 [mm]
Empty weight 21,000 [kg]
Payload - road
19,000 [kg]
Payload - offroad
19,000 [kg]
Gross Weight - road 40,000 [kg]
Gross Weight- offroad 40,000 [kg]
Towed Weight, Max
25,000 [kg]

Gradient
65 [%]

Fording depth
1300 [mm]

Obstacle height, max
800 [mm]

Ditch depth, max
1,400 [mm]

Surface loading
1,6 [kp/cm²]
Tyre Pressure
1,0 - 3,5 [kp/cm²]
Tyres
1500 x 600 - 635
Maximum Speed
60 [km/h]

Cruise Speed
45 [km/h]
Range on internal fuel
1525/450 [km]


MAZ-543 Uragan Powerplant/Systems Specifications
Parameter Type/Metric Magnitude [unit] Type/Imperial Magnitude [unit]
Powerplant
D12A-525, V12, liquid cooled diesel

Max Power
386 / 2100 [kW/RPM]
525 / 2100 [SHP/RPM]

Max Torque
220 / 1400 [kpm/RPM

Displacement
38 800 [cm³]
Tyre
1,0 - 3,5 [kp/cm²]
Electrical System
24 [V]

Batteries
24 [V] 4 x 70 [Ah]

Alternator
3 [kW]

Starter Motor
11.0/15.0 [kW/SHP]

Fuel Tanks
2 x 260.0 [litre]

Source: http://www.militaertechnik-der-nva.de/Katalog/Katalog2Kfz/MAZ543/MAZ543.html; http://legion.wplus.net/guide/army/tr/maz543.shtml



MAZ-543M/7910 chassis dimensions and layout.



MAZ-79100 series tow tractor. The shorted aft chassis and closer spacing of the rear axles is prominent.





The MZKT-79292 is a 10 x 10 MZKT-7930 derivative intended for heavyweight TEL applications, and is a direct competitor to the BAZ-6909 10 x 10 variants (© 2011 Michael Jerdev)



A 5P85SE TEL during a military parade (above). Just aft of the driver cabin is the stowed telescoping mast for the datalink system. S-300PMU2 5P85SE  TEL deployed (below, Said Aminov, Vestnik PVO).










S-300PS 5P85S TEL



5P85SE TEL
(© Miroslav Gyűrösi).


Transporters, Transloaders, Support Vehicles



MAZ-537 Heavy Tow Tractor



KET-T heavy recovery vehicle based on the 1960s MAZ-537 artillery and missile tow tractor., the latter well known as a tow vehicle for larger ballistic missiles. Despite the age of this vehicle it continues to be used to tow the NKMZ 40V6M/MD mobile radar masts (© 2011, Vitaliy Kuzmin).



Systems: NKMZ 40V6M, 40V6MD mobile mast systems for Tin Shield, Flap Lid, Tomb Stone, Grave Stone and Clam Shell.

Характеристики МАЗ-537 МАЗ-537А КЗКТ-537Л
Колесная формула 8x8
Число мест в кабине 4
Грузоподъемность, кг - 15000 16000*
Снаряженная масса, кг 21600 22500 н/д
Полная масса, кг - 37500 40000**
Масса буксируемого прицепа/
полуприцепа, кг
65000*** 75000*** 200000
Длина, мм 9130 9291
Ширина, мм 2885 3100
Высота, мм 2880
Колесная база, мм 1700+2650+1700
Колея колес, мм 2200
Дорожный просвет, мм 500
Габаритный радиус поворота, м 16,5
Двигатель (тип) Д12А-525 (Д, V12) ЯМЗ-240НМ-1Б (Д, V12)
Рабочий обьем, см3 38880 22300
Мощность двигателя, л.с. (об/мин) 525 (2100) 500 (н/д)
Крутящий момент, кГм (об/мин) 220 (1200..1400) н/д
Расход топлива на 100 км, л 125 100
Запас хода, км 1525 н/д
Запас топлива, л 2 x 420
Максимальная скорость, км/ч 55,0 60,0 55,0
Преодолеваемые препятствия:
- глубина брода
- подъем

1,3 м
15°

1,3 м
23°

1,3 м
н/д
 н/д — нет данных
 * масса штатного балласта
 ** со штатным металлическим балластом
 *** на грунте — 30000 кг
Source: Russkaya Sila, URI:http://legion.wplus.net/guide/army/tr/maz537.shtml


MAZ-543M MOBD Accommodation and Generator Vehicle


The MAZ-543M MOBD (Машина обеспечения боевого дежурства) is a support vehicle used with S-300P series batteries deployed in remote areas. It is a fully mobile accommodation vehicle for relief crews, including bunks, a mess and kitchen area, and self contained power generator. Four 30 kiloWatt generators are housed in the forward module, with 4 tonnes of fuel. The aft module contains a galley, food storage, a dining area, two four person bunk compartments, a weapons locker, and an air conditioning system. A number of variants were developed for the RVSN including mobile battery command posts (© 2011, Vitaliy Kuzmin).



Above, below: side and aft views (© 2011, Vitaliy Kuzmin).




5T58 Missile Transporter / KrAZ-260B



5T58 S-300PS/PMU transporter towed by KrAZ-260B (Image by Miroslav Gyűrösi).

While the 5T58 series transporters are typically listed as a missile transporter, the design has been used to also move generators, radar heads, 40V6MD upper mast segments, and a range of other heavy missile battery components. The design appears to be a direct evolution of the 5T53 Transporter/Loader, developed for the earlier S-200VE Vega / SA-5B Gammon.

5T58-2 Missile Transporter / BAZ-6402-015



Late model 5T58-2 S-400 transporter towed by BAZ-6402-015 tractor
(© 2011 Vitaliy V. Kuzmin).



Late model 5T58-2 S-400 transporter towed by BAZ-6402-015 tractor (image © 2011 Michael Jerdev).



(image © 2011 Michael Jerdev)



(image © 2011 Michael Jerdev)



(© 2011 Vitaliy V. Kuzmin)



Detail of 5T58-2 (image © 2011 Michael Jerdev)





The 5T58-2 missile transporters used with S-400 systems are towed by the BAZ-6402-015 tractor (image © Miroslav Gyűrösi).


NPP Start 22T6/22T6E2 Transloader



The NPP Start 22T6E2 Missile Transloader is supplied now on the 8 x 8 Ural 532301 which is also used for the new S-400 / SA-21 55K6E command post (NPP Start).

The 22T6 family of transloaders are a specialised design built to transfer S-300P family missile launch tubes between TELs and transporters, such as the 5T58 or older 5T99. Early variants were supplied on the KrAZ-260 6 x 6 chassis, later variants the 8 x 8 Ural 532301. This design replaces a range of generic cranes used prior to its deployment.



Model of the KrAZ-260 hosted 22T6E transloader (NPP Start).



An S-300PMU 5P85SU TEL being reloaded by a 22T6E transloader (via valka.cz).




KrAZ-260 Tractor



KrAZ-260B tow tractor with deployed 5P85TE TEL.

The Ukrainian built KrAZ-260 series tow tractor has been one of the most widely used with later model S-300PMU series systems. It has been supplanted in the latest variants by the 6 x 6 BAZ-64022 tractor.  Typical KrAZ-260 configurations are powered by a 300 SHP turbocharged V8 diesel.

Specifications
Грузоподъемность, (без лебедки) 9500 кг.

Снаряженная масса (без лебедки и дополнительного снаряжения) 11750 кг.
В том числе:
на переднюю ось 5740 кг.
на тележку 6010 кг.

Полная масса 21475 кг.
В том числе:
на переднюю ось 6320 кг.
на тележку 15155 кг.

Допустимая полная масса прицепа:
по всем видам дорог и местности 10000 кг.
по дорогам с твердым покрытием 30000 кг.

Макс. скорость автомобиля 80 км/ч.
То же, с прицепом полной массой 10000 кг 80 км/ч.
Время разгона атомобиля до 60 км/ч 40 с.
Выбег автомобиля с 50 км/ч 650 м.
Макс. преодолеваемый подъем автомобилем 58 %
То же, с прицепом полной массой 10000 кг 32 %
Тормозной путь автомобиля с 40 км/ 17,2 м.
То же, автопоезда 18,4 м.

Контрольный расход топлива автомобиля, л/100 км, при скорости 60 км/ч 38,5 л.
Глубина преодолеваемого брода с твердым дном при номинальном давлении воздуха в шинах 1,2 м.

Радиус поворота:
по внешнему колесу 13,0 м.
габаритный 13,5 м.
Двигатель.
Мод. ЯМЗ-238Л. дизель с турбонаддувом V-образный 8-цил., 130x140. 14,86 л, степень сжатия 1 5 , 2 , порядок работы 1-5-4-2-6-3-7-8, мощность 220 кВт (300 л.с.) при 2100 об/мин, крутящий момент 1079 Н-м (110 кгс-м) при 1500 об/мин. ТНДВ - 8-секционный, золотникового типа, с т°пливоподкачивающим насосом низкого давления, муфтой опережения впрыска топлива и всережимным регулятором частоты вращения. Форсунки - закрытого типа. Воздушный фильтр - сухой, со сменным фильтрующим элементом и индикатором засоренности. Двигатель оснащен электрофакельным устройством (ЭФУ) и предпусковым подогревателем ПЖД-44МБУ.
Source: autosoft.ru



Ural 375 Tractor



Ural 4320 series flatbed, evolved from the 375 series (Ural).

The Ural 375 series 6 x 6 tractor was often used to tow S-300PT battery components. Variants remain in use for towing trailer mounted components of later S-300P variants. The Ural 375 series was supplanted by the newer production Ural 4320, with a 210 SHP engine.

Параметры Урал-375 Урал-375Д Урал-375A Урал-375С
Грузоподъемность, т 5,0/4,5* 5,8 5,5**
Вес буксируемого прицепа или полуприцепа с грузом, т 10,0/5,0*** 12,0
Масса снаряженного автомобиля, кг 8000/8400* 7100 7700
Полный вес автомобиля, кг**** 13200/13300* 19700*****
Габаритные размеры, мм:
- длина
- ширина
- высота по кабине
- высота по тенту кузова

7350
2690
2680
2980

8000
2500
2680
-

6990
2500
2680
-
База, мм 4200
Колея всех колес, мм 2000
Клиренс, мм
- под передним мостом
- под задними мостами

400
400
Наименьший радиус поворота по колее переднего колеса, м 10,5
Углы въезда, съезда, град:
- передний
- задний

44
40

44
65
Максимальная скорость, км/ч 75 65
Путь торможения со скорости 40 км/ч, м 15 13
Контрольный расход топлива, л/100 км 48 63
Запас хода по контрольному расходу топлива, км 750 625 650
Запас топлива, л
- основной бак
- дополнительный

300
60

300
-

300
110
Двигатель V-образный, 8-цилиндровый, четырехтактный, карбюраторный, верхнеклапанный
ЗиЛ-375
Рабочий объем, л 6,959
Степень сжатия 6,5
Максимальная мощность л.с. (об/мин) 180 (3200)
Макс. крутящий момент, кгм (об/мин) 47,5 (1800)
Электрооборудование батарейное 12 В
Сцепление сухое, двухдисковое с периферийными пружинами, привод рычажный от педали
Коробка передач ЯМЗ-204У, механическая, трехходовая, с пятью передачами для движения вперед и одной назад, с синхронизаторами на второй, третьей, четвертой и пятой передачах
Передаточные числа КПП 6,17; 3,40; 1,79; 1,0; 0,78; задний ход - 6,69
Главная передача Двойная, пара конических шестерен со спиральным зубом и пара косозубых цилиндрических шестерен
Передаточное отношение 8,9:1
Раздаточная коробка Механическая, двухступенчатая с цилиндрическим блокируемым межосевым дифференциалом, распределяющим крутящий момент между передним мостом и тележкой задних мостов в отношении 1:2
Передаточное отношение
- высшая передача
- низшая передача

1,30:1
2,15
Карданная передача Открытая, четырьмя валами с шарнирами на игольчатых подшипниках
Колеса Специальные, с разъемными ободами, коническими полками и распорным кольцом
Шины, размер ОИ-25, 14.00—20
Тормоза Открытого типа, колодочные на всех колесах
Рабочий привод Пнеммогидравлический: для переднего и среднего мостов - совместный, для заднего моста - отдельный
Ручной тормоз Установлен на выходном валу раздаточной коробки, барабанного типа с внутренними колодками; привод сблокирован с тормозным краном ножных тормозов для затормаживания прицепа на стоянке
Рулевой механизм, тип Левого расположения, с гидравлическим усилителем, двухзаходный червяк и зубчатый сектор
Передаточное отношение 21,5:1
Кабина Трехместная, металлическая с мягким верхом, с откидными рамками ветрового и дверных окон Трехместная, цельнометаллическая с глухим ветровым окном, опускными стеклами и поворотными форточками дверей
Платформа Металлическая с задним откидным бортом, оборудована откидными скамейками и съемным тентом с дугами; боковые и передний борта надставные решетчатые -
Внутренние размеры платформы, мм
- длина
- ширина
- высота борта

3900
2430
872
-
 * Без лебедки/с установленной лебедкой.
 ** Максимальная нагрузка на седельное устройство.
*** При движении по дорогам с твердым покрытием/по грунтовым дорогам и бездорожью.
**** В т.ч. вес трех человек в кабине (300 кг).
***** Общий вес автопоезда.
Source: Russkaya Sila







KrAZ-255 Tractor



KrAZ-255 flatbed (Wikipedia commons image).

The Ukrainian KrAZ-255 series 6 x 6 tractor was widely used to tow S-300PT battery components. Typical configuration is fitted with a 240 SHP diesel engine. Variants remained in use for towing trailer mounted components of later S-300P variants, but were mostly supplanted by the newer KrAZ-260 series.

Specifications

Грузоподъемность (без лебедки)
8020 кг.
Снаряженная масса (с дополнительным снаряжением)
В том числе:
на переднюю ось 4920 кг.
на тележку 6250 кг.
11170 кг.
Полная масса
В том числе:
на переднюю ось 5190 кг.
на тележку 14225 кг.
19415 кг.
Глубина преодолеваемого брода с твердым дном при номинальном давлении воздуха в шинах  1,0 м
Радиус поворота:
по внешнему колесу
габаритный 

13,5 м.
14,2 м.
Грузоподъемность (без лебедки)  8020 кг.
Снаряженная масса (с дополнительным снаряжением)
В том числе:
на переднюю ось 4920 кг.
на тележку 6250 кг.
11170 кг.
Полная масса
В том числе:
на переднюю ось 5190 кг.
на тележку 14225 кг.
19415 кг.
Допустимая полная масса прицепа по всем видам дорог и местности  10000 кг
Допустимая полная масса прицепа по дорогам с твердым усовершенствованным покрытием 30000 кг
Макс.скорость автомобиля
71 км/ч
То же, автопоезда с прицепом полной массой 10 т 71 км/ч
Время разгона автомобиля до 60 км/ч  40 с
Выбег автомобиля с 50 км/ч  650 м
Макс.преодолеваемый подъем автомобилем 58 %
То же, автопоездом с прицепом полной массой 10000кг  32 %
Тормозной путь автомобиля с 40 км/ч:
автомобиля 17,2 м
автопоезда 18,4 м
Контрольный расход топлива автомобиля, л/100 км, при скорости 60 км/ч  35,3 л
Глубина преодолеваемого брода с твердым дном при номинальном давлении воздуха в шинах  1,0 м
Радиус поворота по внешнему колесу 13,5 м
Радиус поворота габаритный  14,2 м
Двигатель: Мод. ЯМЗ-238М2, дизель, V-o6p. (90°), 8-цил., 130x140 мм, 14,86 л, степень сжатия 16,5, порядок работы 1-5-4-2-6-3-7-8, мощность 176 кВт (240 л.с.) при 2100 об/мин, крутящий момент 883 Н-м (90 кгс-м) при 1450-1600 об/мин; ТНВД - 8-секционный, золотникового типа, с топливоподкачивающим насосом низкого давления, муфтой опережения впрыска топлива и всережимным регулятором частоты вращения. Форсунки - закрытого типа. Воздушный фильтр - сухой, со сменным фильтрующим элементом и индикатором засоренности. Двигатель оснащен предпусковым подогревателем ПЖД-44МБУ теплопроизводительностью 32000 ккал/ч.





KrAZ-255 flatbed (Wikipedia commons image).

BZKT BAZ-69092-021



BAZ-69092-021 Flatbed  (© 2011 Vitaliy V. Kuzmin).

The BAZ-69092-021 is a designated support vehicle for S-400 batteries, intended to tow equipment such as the 5I57A power generator, 63T6 mains power converter, and other equipment. It is likely to be used for the same purpose in S-500 batteries.

Наименование Значения
Колесная формула, 8х8.1
Полная масса буксируемого полуприцепа, т 15 (самолетов - 50)
Полная масса автопоезда, т, не более 47,500/82,500
Балласт, т 11
Сцепление однодисковое диафрагменное, ЯМЗ-184.10
Коробка передач, 9 передач вперед, 1 назад, ЯМЗ-2393-03
Подвеска I и II осей, независимая, двухторсионная с амортизаторами на каждом колесе
Подвеска III и IV осей, комбинированная, независимая одноторсионная для нижних рычагов и балансирная, рессорная для верхних
Шины с регулируемым давлением, радиальные (1350х550-533Р), ИД-370
Минимальный радиус поворота, м 13
Максимальная скорость, км/ч 70
Запас хода по контрольному расходу топлива, км 1000
- по бездорожью, 15,0
- по дорогам с твердым покрытием, 50,0
Габаритные размеры
Длина, мм 10401
Ширина, мм 2750
Высота, мм 3190
Двигатель
Марка двигателя, ЯМЗ-8424.10
Мощность, л.с. 470



BAZ-69092-021 Flatbed  (© 2011 Vitaliy V. Kuzmin).


5I57/5I57A Mobile Diesel Power Generator



(Valka.cz).

Variants of the 5I57/5I57A have been used across a wide range of S-300P derivatives to provide independent electrical power at static SAM site installations. Typically it is towed by the standard battery general purpose truck, including the KrAZ-255, KrAZ-260, Ural-375, Ural-4320, and in later S-400 batteries, the BAZ-69092-012 flatbed.


63T6/63T6A Mobile Mains Grid Power Converter

Variants of the 63T6/63T6A have been used across a wide range of S-300P derivatives to provide electrical power at static SAM site installations. The system converts and stabilises local mains grid power to a format compatible with battery components. Typically it is towed by the standard battery general purpose truck, including the KrAZ-255, KrAZ-260, Ural-375, Ural-4320, and in later S-400 batteries, the BAZ-69092-012 flatbed.



Technical Report APA-TR-2008-0601-A





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