S-300P/S-400 Vehicles

Last Updated: Sun Aug 29 16:43:38 UTC 2010

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

Technical Report APA-TR-2008-0601-A

by Dr Carlo Kopp, SMAIAA, MIEEE, PEng
June 2008
Updated February 2010
Text © 2008, 2010 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 (© Miroslav Gyűrösi).

Background/Introduction
S-300P Variant TEL Design
- TEL Datalink Antennas
S-300P/S-400 Transporter Erector Launcher Vehicles

Background/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.

S-300P 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	5P85SE2	5P85T2/TE2	Russian Export
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.

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). This design provides high mast elevation, and directional emission, requiring the TEL 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).

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 Transporter Erector Launcher Vehicles

5P90SE Self Propelled Transporter Erector Launcher

5P90TMU Towed Transporter Erector Launcher

Systems: S-400

The 5P90 series are a reported new TEL design for the S-400 Triumf / SA-21 SAM system. It is expected that both designs will be based on variants of the BAZ-69092 "Voshchina 1" series of military trucks, used currently with the 5P85T2/TE2 TEL supplied with the S-400 and recently exported S-300PMU-2 models. To date no imagery has been released.

5P85TM/T2/TE2 Towed Transporter Erector Launcher

Systems: S-400

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.

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).

BAZ-64022 tractor (above, below).

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 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.

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).

A support vehicle used with S-300PMU batteries deployed in remote areas is a fully mobile accommodation vehicle for relief crews, including bunks, a mess and kitchen area, and self contained power generator.

5T58 Missile Transporter

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