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SA-10 Surface-to-air S-300PMU missile launcher. The weapon is carried and vertically launched from a dedicated four-round capacity transporter-erector launcher vehicle based on the MAZ-7910 ( 8 x 8 ) truck chassis.
SA-12A Surface-to-air missile launcher in a dual role as anti-missile or anti-aircraft with a max range of 75 to 90 km. The 9A83-1 tracked vehicle carries four 9M83 SA-12a GLADIATOR missiles.
SA-20 The 9M96 missile is designed to destroy aircraft and air- delivered weapons at ranges in excess of 120 km. The missile is small-- considerably lighter than the ZUR 48N6Ye used in the S-300PMU1 systems and the Favorit. The missile is equipped with an active homing head and has an estimated single shot kill probability of 0.9 for manned aircraft and 0.8 for unmanned maneuvering aircraft. a gas-dynamic control system enables the 9M96 missile to maneuver at altitudes of up to 35 km at forces of over 20g, which permits engagment of non- strategic ballistic missiles. A mockup of the missile was set up at an Athens arms exhibition in October 1998. One 9M96 modification will become the basic long-range weapon of Air Force combat aircraft, and may become the standardized missile for air defense SAM systems, ship-launched air defense missile systems, and fighter aircraft.
S-400 (SA-20 Triumf)
Alternate Name: SA-20 Triumf
Country: Russia
Basing: Land
Details
The S-400, also known by its NATO designation, SA-20 Triumf, is an advanced Russian surface-to-air missile system. Once operational, it will be able to destroy aircraft, cruise missiles, and short- and medium-range ballistic missiles at ranges of up to 400 kilometers. The Russians eventually plan to phase out their existing S-200 (NATO: SA-5 Gammon) and S-300P (NATO: SA-10 Grumble) systems and replace them with S-400 complexes.
A standard S-300P
tracked 8 X 8 MAZ-7910 truck chassis launcher originally designed to carry four 5V55 or 48N6 missiles would now be used to transport up to 16 9M96 missiles. In addition, the S-400 would use the S-300P control complex and multifunctional radar, thus allowing for a smooth, cost-efficient transition between the two systems.
The differences are all in the Launcher, TELAR, Radars, and missiles.