Originally Posted By: ePap


Just go back to page 39 and read ,not only with eyes ...

Variants
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9K33 "Osa" (US DoD designation SA-8A "Gecko") began development in 1960 and was introduced in 1971-1972 with four exposed 9M33 missiles per TELAR 9A33B and a maximum range of 12 km (7.5 mi).
9K33M "OSA-M" (NATO reporting name SA-N-4 "Gecko") was introduced in 1972 and is the naval version of the system with two 9M33M missiles on a Zif-122 retractable rotating launcher and improved performance. It has been installed on Gepard class frigate, Kara class guided missile cruisers, Kiev class VTOL cruisers and also the Kirov, Slava and Krivak classes.
9K33M2 "Osa-AK" (US DoD designation SA-8B "Gecko Mod-0") with TELAR 9A33BM2 was introduced in 1975 with the new six-missile box launcher, each 9M33M2 missile being a sealed round.
9K33M3 "Osa-AKM" (US DoD designation SA-8B "Gecko Mod-1") with TELAR 9A33BM3 and missiles 9M33M3 was introduced in 1980 with the maximum range extended to 15 km (9.3 mi) and maximum altitude to 12 km (40,000 ft) as explained above. Most OSA-AKM systems also feature an IFF antenna.

Missiles
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Engagement range for the early versions is approximately 2–9 km (1.3-5.6 miles) and engagement altitudes of between 50–5000 m (164-16,400 ft). The 9M33M2 "Osa-A" missile extends the ranges out to 1500-10000m (1-6.2 miles) and engagement altitudes to 25–5000 m (82-16,400 ft). The 9M33M3 missile greatly enhances the altitude engagement envelope to 10–12000 m (33-42,500 ft), and as such are also able to fly further (about 15 km/9 miles) but the system is not able to engage targets at longer ranges, due to other factors such as the radar tracking of the missiles. The system is designed for use primarily against jet aircraft and helicopters in any kind of weather.

The 9M33 missiles are 3.158 m (10.3 ft) long, weigh 126 kg (278 lb) and use command guidance. There is also a backup low-light optical tracking system for heavy ECM environments. The latest 9M33M3 missiles have an increased total weight of 170 kg (375 lb) in order to provide the extended range coverage and larger warhead. Propulsion is provided by a dual-thrust solid fuel rocket motor. Both versions feature a missile speed of around Mach 2.4 (peaking at around Mach 3) for a maximum target engagement speed of around Mach 1.4 for the original missile and Mach 1.6 for the M2\M3 missiles. The warhead for the initial and M2 versions weighs 19 kg (42 pounds), increased to 40 kg (88 lb) in the M3 version to improve performance against helicopters. All versions have impact and proximity fuzes.


http://en.wikipedia.org/wiki/9K33_Osa

all i know

Last edited by farokh; 07/08/13 04:29 PM.