| SA-12 S-300V Gladiator MIssile - 393 sec
The missile is designed to engage both modern and prospective air targets, including strategic, tactical and naval aircraft, strategic cruise missiles, air-launched missiles, tactical and battlefield ballistic missiles and other air attack weapons over a wide range of combat environments.
The 5V55R is a single-stage missile employing the normal aerodynamic configuration, with control surfaces unfolded after launch.
The missile is kept in a hermetically sealed launch canister and need not be tested and adjusted during its service life.
The missile is equipped with a highly efficient solid-propellant motor and comprises sections housing a radio direction finder, onboard control units (made as a monoblock), high-explosive fragmentation warhead, solid-propellant motor and control surface actuators.
The missile is launched vertically by the canister catapult without a preliminary turn of the launcher toward the target.
After ignition of the motor, the missile is tilted in the required direction depending on the target position.
The missile employs the track-via-missile guidance principle.
The high maneuverability of the missile and powerful high-explosive fragmentation warhead provide effective target destruction.
Auteur : galbaldy
Tags:Russian Soviet army military airdefense SA-12 S-300V Gladiator AAA missile U2
 | | SA-15 Gauntlet / Tor 9K330 Missile System - 347 sec
The 9K331 Tor [SA-15 GAUNTLET land-based, SA-N-9 naval version] low-to-medium altitude SAM system is capable of engaging not only aircraft and helicopters but also RPVs, precision-guided weapons and various types of guided missiles. The HQ-17 is a copy of Tor-M1, that China will use it to replace the aging HQ-61 SAMs, will enter service around the year 2005. Although it is an autonomous system it can be interfaced into an integrated air defense network. SA-15b is designed to be a completely autonomous air defense system (at division level), capable of surveillance, command and control, missile launch and guidance functions from a single vehicle. The basic combat formation is the firing battery consisting of four TLARs and the Rangir battery command post. The TLAR carries eight ready missiles stored in two containers holding four missiles each. The SA-15b has the capability to automatically track and destroy 2 targets simultaneously in any weather and at any time of the day.
Effective range limits are from 1500 to 12000 m with target altitude limits being between 10 and 6000 m. The maximum maneuvering load factor limit on the weapon is 30 g.
The missile launcher consists of a box container extending down below the level of the hull top, holding two groups of four ready to fire missiles in the vertical position. Each missile is in a maintenance-free factory-sealed container-launcher box. The system is reloaded by a dedicated transportation/loader vehicle.
The 3D pulse Doppler electronically beam steered E/F-band surveillance radar provides range, azimuth, elevation and automatic threat evaluation data on up to 48 targets for the digital fire control computer processing system. Automatic track initiation can be performed on the 10 most dangerous targets, which are categorized and prioritized in order of threat for engagement. The operator reconfirms the highest priority target choice and tracks this target before firing the missile. The maximum radar range is stated as 25 kilometers, but the rapid five to eight second reaction time [including fire control target prioritization] suggests a somewhat greater range. The radar antenna, on top of the turret, is swung through 90º to the horizontal position for travel. Target radar surveillance is carried out on the move but the vehicle would normally come to a halt for missile launch.
The phased-array pulse Doppler G/H-band tracking radar is located at the front of the turret. This electronically steered radar is capable of simultaneously tracking two targets traveling at speeds of up to 700 km/h in all weather conditions, and countering threat ECM operations. The antenna assembly can be folded down for travel.
Mounted on the top left of this radar is a small vertical pointing antenna which serves to initially acquire the missile after launch before it is handed over to the main tracking/guidance system. On the lower right side of the tracking radar is an automatic TV tracking system with a range of 20000 m that complements the tracking radar and enables the system to operate in a heavy ECM environment.
The Tor is not amphibious although it is airportable. An NBC system is fitted as standard as is a built-in training system. The chassis of the vehicle is almost identical to that used for the 2S6 self-propelled hybrid air defense system and is based on the GM-569 tracked vehicle. The three man crew consists of the vehicle commander, system operator and vehicle driver, seated at the front of the vehicle with the large box-like unmanned turret in the center and the engine compartment at the rear. This arrangement is similar to that of the Kub (SA-6) and Shilka (ZSU-23-4) vehicles. The vehicle suspension consists of six dual rubber tired roadwheels with the idler at the front, drive sprocket at the rear and three return rollers.
An auxiliary gas turbine powers a 75 kW generator, allowing the main diesel engine to be shut down when the system is deployed to conserve fuel.
Auteur : galbaldy
Tags:Russian Soviet army military airdefense SA-15 Tor 9K330 missile U2 Gauntlet PVO AAA gun artillery
| | air defense ZSU-23 Shilka Tunguska - 354 sec
The Shilka ZSU-23-4 [ZSU = Zenitnaya Samokhodnaya Ustanovka - Anti-aircraft Self-Propelled Gun] is a Self-Propelled Anti-Aircraft Gun (SPAAG) featuring a prominent radar dish that can be folded down mounted on a modified PT-76 chassis. ZSU 23-4 Shilka, is capable of acquiring, tracking and engaging low-flying aircraft (as well as mobile ground targets while either in place or on the move). Employed in pairs 200 meters apart, 400 meters behind battalion leading elements, it is commonly used to surpress ATGM launch sites, such as TOW vehicles. The armament consists of four 23mm cannon with a maximum slant range of 3,000 meters. Ammunition is normally loaded with a ratio of three HE rounds to one AP round. Resupply vehicles carry an estimated additional 3,000 rounds for each of the four ZSUs in a typical battery. Recent (October 1997) information details ZSU-23-4 updates/modernization being offered by the Ukrainians that include: a new radar system replacing the GUN DISH radar, plus a sensor pod believed to include day/night camera, and a laser rangefinder; and mounted above radar/sensor pod is a layer of six fire-and-forget SAMs, believed to be Russian SA-18/GROUSE.
The ZSU-23-4 is a fully integrated, self-propelled antiaircraft system with four liquid-cooled 23-mm automatic cannons mounted on the front of a large, flat, armored turret. The chassis has many components borrowed from other Soviet armored vehicles, and the suspension system resembles that of the PT-76 and ASU 85 (six road wheels and no track support rollers). The driver sits in the left front of the hull, and the rest of the crew (commander, gunner, and radar operator) are located in the turret. The GUN DISH fire control radar mounted on the rear of the turret can be folded down during travel.
A number of different ZSU-23-4 models have been produced. These are primarily distinguishable externally by the types of stowage boxes on the turret and minor modifications in the mounting of the guns.
CAPABILITIES:
A platoon of four ZSU-23-4s is assigned, along with four SA-9/GASKIN SAM systems, to the antiaircraft battery of motorized rifle and tank regiments to cover the deadspace of the SA-6/GAINFUL in the division air defense umbrella. Two ZSU-23-4s usually will be in support of each of the two first-echelon battalions, each weapon normally separated by 200 meters, typically traveling 400 meters behind the battalion's leading elements.
The ZSU-23-4 is not amphibious, but has a fording capability of just over one meter. During river assault operations, the ZSU-23-4s would be ferried to the far bank immediately after the leading companies.
The ZSU-23-4 has the capability to both acquire and track low-flying aircraft targets, with an effective AA range of 2,500 meters. It also is capable of firing on the move because of its integrated radar/gun stabilization system. The high frequency operation of the GUN DISH radar emits a very narrow beam that provides for excellent aircraft tracking while being difficult to detect or evade. However, such a frequency also dictates a limited range, which can be compensated for by linking the system to other long-range acquisition radar in the area. The ZSU-23-4 also can be used against lightly armored ground vehicles.
The four guns are water cooled and have a cyclic rate of fire of 800 to 1,000 rounds per minute each. However, the guns are normally fired in bursts (2-3 rounds per barrel) to reduce ammunition expenditure and prolong barrel life. Each ZSU-23-4 carries about 2,000 rounds onboard. Supply trucks, which follow the ZSUs at a distance of 1.5 to 2.5 km, carry an estimated additional 3,000 rounds for each of the four ZSUs. Electronic target acquisition, tracking, and ranging are automated, and an onboard computer determines superelevation and azimuth lead. Conventional optical sights also are available. Two types of ammunition normally are mixed at a ratio of three Frag-HE-T rounds per one API-T round. An HEI-T round also may be fired.
TheZSU-23-4can be airlifted bytheAN-22 or II-76. The crew of the ZSU-23-4 is afforded a degree of protection by the thin armor (maximum thickness 9.4 mm in the hull, 8.9 in the turret). Collective NBC protection is provided by a radiation detection and warning system and an air filtration and overpressure system.
LIMITATIONS:
Heavy machine gun fire can penetrate the hull and turret. Tread and road wheels are vulnerable to artillery fire. HE fragmentation can penetrate the armor, destroy the radar dish, or rupture the liquid coolant sleeves of the 23-mm cannons. The system also is vulnerable to ECM.
Auteur : galbaldy
Tags:Russian Soviet army military airdefense ZSU-23 missile U2 Tunguska PVO AAA gun artillery
| | S-200 SA-5 GAMMON Missile - 20 sec
The task of defeating the carriers of cruise missiles, jammers, aircraft of strategic aviation at maximum ranges and heights was solved between 1963 and 1967 with the creation of the S-200 system. Together with the development of many new scientific and technical solutions for the S-200 system, A.A. Raspletin was attached the fundamental importance to the creation of self-homing head for the anti-aircraft guided missile. In the accepted for the armament system S-200 the anti-aircraft guided missile was for the first time equipped with homing equipment.
The S-200 SA-5 GAMMON is a medium to high -altitude surface-to-air missile system. The single-stage missile has four jettisonable, wraparound solid propellant boosters, each of which is is 4.9 m long and 0.48 m in diameter with a single fin spanning 0.35 m from the booster body. The missile is 10.72 m long overall with a wing span of 2.85 m. The main body is 0.85 m in diameter and has a solid fuel dual thrust sustainer rocket motor.
Each missile battalion has one 320 km range P-35M BARLOCK-B E/F-band target search and acquisition radar with an integral D-band IFF system, one 270 km range SQUARE PAIR H-band missile guidance radar, and six trainable semi-fixed single rail launchers.
The missile's minimum range of 60 km is due to the booster burn time and jettison requirements, limiting the system to engagements against relatively large unmaneuverable targets at ranges up to 250 km. Guidance beyond the 60 km booster jettison point is by course correction command signals from the SQUARE PAIR radar with the S-200's own active radar terminal homing seeker head activated near the projected intercept point for final guidance.
The large HE warhead is detonated either by a command signal or the onboard proximity fusing system. When fitted with a nuclear warhead only the command detonation option is used.
Auteur : galbaldy
Tags:Russian Soviet army military airdefense sa-5 s-200 missile U2 angara vega dubna
| | SA-3 GOA S-125 Pechora Missile - 34 sec
The S-125 NEVA-M (SA-3 GOA) is a surface-to-air anti-aircraft short-range system designed for destruction of aircraft, cruise missiles, assault helicopters and other air targets at ground, low and medium altitudes. The development of air weapon systems and the need for the protection of the most important objects in the territory of the country required the development of the mobile systems of rocket weapon, capable of resisting massed attacks of aviation and cruise missiles, including at the maximally low altitudes of their combat employment. Solution of the problems indicated was achieved/reached during the creation of zenith rocket systems S-75 and S-125, which were developed between 1957 and 1961 under design project leader A.A. Raspletin's management.
US intelligence imagery at Kapustin Yar in late 1959 revealed two probable R&D sites, each of which consisted of four launch pads. A possible launcher on one of the pads held two missile-like objects about 20 feet long. US intelligence subsequntly identified more than 35 sites of this type in the USSR between late 1961 and 1964, usually near SA-1 or SA-2 sites. The initial SA-3A GOA Mod 0, deployed in 1961, includes command guidance throughout the missile's flight. The subsequent SA-3B GOA Mod 1, first deployed in 1964, incorporated an improved guidance system. The missile's ability to dive allows it to be used against surface targets and naval vessels.
The S-125 is fired from trainable launchers which are normally fixed, but can be relocated. The crew loads the missiles with the aid of a conveyor onto the ground-mounted, trainable launcher for firing, with both twin and quadruple launchers in use. A pair of missiles are carried in tandem on a modified truck or tracked vehicle. The S-125 is normally transported from battalion storage areas on modified ZIL-131 (6 x 6) or ZIL-157 (6 x 6) trucks and loaded onto the launchers. Approximately one minute is required to load the missiles onto the launch rails, but nearly an hour is required between missile launches due to missile preparation, truck transit and other reloading procedures.
The modernised surface-to-air missile system "Pechora-2M" is an effective weapon against low-flying and small-size targets. Noise-protection equipment newly introduced will provide detection, tracing, and hitting targets in conditions of intensive influence of all kinds of radio noise and counter-measures. New teleoptical drift indicator provides targeting in conditions of radio-silence in day and night time. Doubling the number of launching pads enlarges fire capability of the system. Substitution of main equipment for modem digital and solid-state one allows to prolong the system life and lower costs {or its repair. Self-testing system introduced simplifies and reduces maintenance time 8-10 otime decrease in the spare parts nomenclature streamlines the order of supplying and lowers expenditures for the system operation. Introduction of telccodc communication equipment, navigation system, and interface applied provide for possibility of receiving radar information from any sources by the missile system. The possibility of mounting the system means upon self-propelled chassis drastically increases the system mobility. Recession of the control cab at large distance from the site centre saves the detachment's life. On the base of modernised technics already available, after moderate expenditures, customers get a modem weapon.
Auteur : galbaldy
Tags:Russian Soviet army military airdefense sa-3 goa s-125 pechora neva missile U2
| | SA-2 GUIDELINE V-75 Missile - 59 sec
The V-75 SA-2 GUIDELINE is a medium to high altitude surface-to-air missile system. This two-stage missile has a large solid propellant booster stage fitted with four very large delta fins. The core stage consists of a storable liquid propellant sustainer rocket motor using inhibited red fuming nitric acid oxidizer and kerosene fuel. A set of four cropped delta-shaped wings are located near the mid-section, with a second in-line set of smaller fixed fins at the nose, and a third in-line set of slightly larger powered control fins at the tail.
The guidance system at an SA-2 site can handle only one target at a time, but can direct three missiles against a target simultaneously. Additional missiles could be fired against the same target after one or more missiles of the first salvo had completed their run. The Soviets apparently believed they must program three or four missiles against each target in order to achieve acceptable kill probabilities.
The 295 kg nuclear warhead used only on the SA-2E variant is believed to have a yield of 15 kT. The other V-75 variants have an internally grooved fragmentation warhead weighs 195 kg (130 kg of which is high explosive) with proximity, contact and command fusing available. This conventional warhead is fitted forward of the main fins and behind the nose-mounted guidance assembly. At medium and low altitudes the kill radius is about 65 meters and the blast radius for severe damage is 100-120 meters. The maximum blast radius against a high altitude target is approximately 250 meters, due to the rarefied atmosphere. The weapon has a accuracy of 75 meters with the large blast radius compensating for system inaccuracies.
The system S-75 participated in the combat operations in Vietnam. On 01 May 1960, near Sverdlovsk, the invulnerable, high-altitude reconnaissance aircraft U-2 which was being piloted by Gary Powers was shot down by an SA-2.
Although there are a variety of arrangement patterns, all sites consist of six launching positions -- usually revetted - deployed around a guidance radar and linked by service roads to facilitate loading. While the sites were permanent installations, all operating components of the system are mounted on wheeled vehicles and are capable of movement by road or raiL
The V-75 was the basic missile defense system for critical urban-industrial areas in the USSR, other than Moscow. The V-75 deployment began on a wide scale since early 1958, with sites located throughout the western part of the Soviet Union and Warsaw Pact countries. Deployment patterns and levels of concentration varied according to the geography, size, and shape of the target area, and the Soviet estimate of the worth of individual targets. Between mid-1958 and 1964 more than 600 SA-2 sites were identified by US intelligence in the USSR, mostly in defense of population centers, industrial complexes, and government control centers.
Most SA-2 sites defended major centers of population and industry. SA-2 defenses were also deployed for the special protection of nuclear materials production and storage facilities. In addition, some key Soviet field forces and long range bomber bases were included in the SA-2 deployment pattern. The construction of sites and the training and activation of firing units was seasonal, with activity at a minimum during the winter months.
The sites in the Moscow area, located within the inner ring of SA-1 sites, were intended to supplement the existing defenses. Deployment of SA-2 installations around Moscow included seven sites as of 1964 as part of a program to supplement the SA-1 system.
Auteur : galbaldy
Tags:Russian Soviet army military airdefense sa-2 guideline v-75 missile U2
| | 2s9 Nona 2s31 Vena 120mm - 591 sec
The gun is capable of delivering aimed direct and indirect fire employing HE 120-mm Russian-made projectiles, and mines of both Russian and NATO standards. Consequently, the gun constitutes a hybrid of a howitzer and mortar that can provide fire support for mechanised infantry sub-units in all types of combat. The auxiliary weapon set comprises a 7.62-mm machine gun mounted on the turret roof, a smoke-screen system, as well as sighting and night-vision devices. Specialists throughout the world appreciate the need to equip high mobility combat units (paratroops, airmobile and naval infantry) with a powerful artillery system that can correspond to ways of their shipment and mobility in terms of their marching and maneuvering characteristics.
Auteur : galbaldy
Tags:laser guided Russian Russia army military artillery Tactical 2s9 2s31 Mortar 120mm Nona Vena
| | SS-21 SCARAB 9K79 Tochka FROG-7 Luna - 370 sec
The SS-21 SCARAB (9K79 Tochka) single-stage, short-range, tactical-ballistic missile is transported and fired from the 9P129 6x6 wheeled transporter erector launcher. It is supported by a tactical transloader (9T218) and a 9T238 missile transporter trailer towed by a ZIL-131 truck. The 9P129 TEL crew compartment is in the forward section and the missile compartment behind. During transport the missile is enclosed with the warhead in a temperature-controlled casing.
The SS-21 SCARAB missile (9M79) has a maximum range of 70 km and a CEP of 160 meters, while the improved composite propellant 9M79-1 (Tochka-U) has a maximum range of 120 km. The basic warhead is the 9N123F HE-Frag warhead which has 120 kg of high explosives. The 9N123K submunition warhead can probably carry either bomblets or mines. The SS-21 can also carry the AA60 tactical nuclear warhead. Other warheads are believed to include chemical, terminally guided warhead, and a smart-munition bomblet warhead. In 1981, the SS-21, a guided missile (providing improvement in both range and accuracy), began replacing the FROG in forward-deployed divisions, and 140 are were deployed as of 1988. Division-level SS-21 battalions were being consolidated into brigades in Soviet armies in East Germany.
Auteur : galbaldy
Tags:MAZ Russian Russia army military rocket missile nuclear truck Theater Tactical SS-21 Scarab Tochka
| | SS-23 Spider 9K714 OKA Missile - 425 sec
In the early 1970s, the Soviet Army sought a replacement for the 9K72 Elbrus (SS-1C `Scud B') system, which had a very slow reaction time [around 90 minutes to prepare and fire] and its poor accuracy when using conventional warheads. The replacement system, codename 9K714 Oka, was developed by KB Mashinostroyenia (Machine Industry Design Bureau) in Kolomna. The new 9K714 system featured a reaction time of under 30 minutes and used the low-maintenance solid-fuel 9M714 missile. The 300 km range of the R-300 (`Scud') was surpassed by the 400 km range of the 9M714/R-400.
In the early 1970s the Warsaw Pact had only a limited ability to strike North Atlantic Treaty Organization (NATO) air bases in Europe. However, by the mid-1980s Soviet forces could strike NATO airfields in all types of weather using tactical ballistic missiles (TBMS) such as the SS-21 and the SS-23. NATO had only limited defense against these weapons, some of which were accurate to within 100 meters. The SS-23 has a range of 310 miles, with speeds of 6,800 miles per hour or Mach 9 that can access most locations in a given theater of war.
The Intermediate-Range and Shorter-Range Nuclear Forces [INF] Treaty was signed on 08 December 1987 and entered into force on 01 June 1988. The fundamental purpose of the INF Treaty was to eliminate and ban US and former USSR (FSU) ground-launched ballistic and cruise missiles, as well as associated support equipment, with ranges between 500 and 5500 kilometers. SS-12 and SS-23 transporter-erector-launcher (TEL) vehicles were eliminated at Stan'kovo.
Auteur : galbaldy
Tags:MAZ Russian Russia army military rocket missile nuclear truck Theater Tactical OKA SS-23
| | Topol-M SS-27 Missile ICBM - 249 sec
The single-warhead Topol-M is an advanced version of the silo-based and mobile Topol intercontinental ballistic missile. The solid-propellant three- stage Topol-M missile complex, with a standardized (silo and mobile) missile, is to become the foundation of the Russian strategic nuclear forces in the 21st century. It is planned to accommodate Topol-M both on self-propelled launchers as well as in silos. High survivability of the mobile complex is achieved by the capability of offroad movement, of a continuous change in location and of a missile launch from any point along the movement route. The Moscow Institute of Heat Engineering (MIT) State Enterprise is the only plant in Russia building such missiles today.
The modernized 45-ton Topol-M is the first strategic missile to be built by Russia without the participation of Ukraine and CIS countries. The flight and design testing of the Topol-M was successfully completed in 1995, and joint flight-testing is continuing, leading to a decision to commence series production. All the launches have been a success, but serial production has not started due to a shortage of funds. On 08 July 1997 the fourth launch of a Topol-M ICBM was successfully made from the Strategic Missile Forces' Plesetsk State Test Site within the framework of joint flight-testing. Work on the new Topol-M ICBM is lagging seriously behind the initial timetable. Defense state order financing for the next decade provides that by 2003 there will be on the order of 250-300 Topol-M missiles in service. A total of 1.5 trillion [old] rubles were included in the 1997 budget for the development of the Topol-M missile complex. The Russian Missile Troops are permitted to have 300 Topol RS-12M mobile missiles under the START II Treaty, and the RVSN must acquire two Topol-M regiments annually up to 2001, which will cost 3.7 billion new rubles. A total of R700 billion would be required to place 450 Topol-M missiles in service by 2005 to maintain parity under START II.
But the present 55 percent funding will permit production of at the very most 10-15 missiles at this facility each year year. As a result the Strategic Missile Troops will have a total of approximately 350-400 ICBM warheads, not the 800-900 which are permited within the framework of the START II Treaty. On 15 April 1998 Acting Prime Minister Sergey Kiriyenko approved a schedule of monthly budget appropriations for the Topol-M, which he noted would make up the core of Russia's strategic nuclear forces. In December 1997, the first two Topol-M systems were put on alert for a trial period with the Taman Division at Tatischevo in the Saratov region. As of late July 1998 two more Topol-M launch sites were completed and were awaiting acceptance trials. The Topol-M missile system is being commissioned in the Russian strategic nuclear forces' grouping regardless of whether heavy missiles are stood down from combat alert duty or not. It is intended that the Topol-M ICBM grouping will comprise an equal number of mobile and silo-launched missiles. Some 90 of the 360 launch silos vacated by the RS-20 ICBM's, which are being stood down from combat alert duty, need to be converted for the latter. Apart from Saratov Oblast the Topol-M systems will be deployed in Valday, the southern Urals, and the Altay.
The Topol-M missiles could be transformed into missiles with multiple reentry vehicles [MIRV's], since their throw weight allows accommodating 3-4 warheads on a missile. The warheads could be taken from some of those ground-based and naval missiles which will be withdrawn from the order of battle in coming years.
Auteur : galbaldy
Tags:MAZ Russian Russia army military rocket missile nuclear truck ICBM Strategic ballistic Topol SS-27
| | Iran-Iraq war documentary - 334 sec
From 1980 to 1988 the two countries fought a brutal war, spurred by arms from the industrialized nations. Truely a forgotten tragedy of our times.
http://www.zmag.org/zmag/articles/ShalomIranIraq.html
Auteur : galbaldy
Tags:Iran Iraq iran-iraq war military history documentary weapons combat crimes battle
| | Russian military sidecar promo video - 179 sec
A URAL Gear-Up Russian military sidecar with engagable 2 wheel drive for offroading. Apparently they also distribute them in the U.S.
http://www.ural.com/
Auteur : galbaldy
Tags:Gear-up URAL IMZ Russia Russian offroad military army motorcycle sidecar promo
| | Russian 8x8 FROG-7 ZIL-135 goes for a test run - 57 sec
Powered by two 7Ltr 180HP petrols with 3 gas tanks, this vehicle was used to transport and reload missiles for the FROG-7
Auteur : galbaldy
Tags:FROG-7 BAZ ZIL Russian Russia army military rocket missile nuclear 8x8 truck offroad petrol diesel
| | Russian 6x6 ZIL-131 Decon truck offroading - 73 sec
ZIL-131 6x6 decontamination truck offroading in U.K.
Auteur : galbaldy
Tags:ZIL truck ZIL-131 6x6 Russia Russian offroad army military decontamination diesel petrol
| | Russian ZIL 6x6 truck goes offroading - 173 sec
ZIL-131 navigates the backroads of the U.K. It's a mass production 6x6 offroad truck used by the Russian army. Surprisingly, it's powered by a petrol engine.
Auteur : galbaldy
Tags:ZIL truck ZIL-131 6x6 Russia Russian offroad army military diesel petrol
| | Russian Kamaz trucks in action at IDEX - 58 sec
Russian Kamaz trucks at Idex-2003 in the UAE. These trucks, along with Czech Tatras are the best in the world.
Auteur : galbaldy
Tags:Kamaz truck IDEX 2003 UAE 4x4 6x6 8x8 army military russian russia diesel petrol
| | Russian Kamaz truck runs exhibition circuit - 55 sec
Russian Kamaz trucks at the arms expo in Nizhny Taghil. These trucks, along with Czech Tatras are the best in the world.
Auteur : galbaldy
Tags:truck Kamaz 4x4 6x6 8x8 russian russia army military 2003 diesel petrol
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