9K33 Osa

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9K33 Osa
(NATO reporting name: SA-8 Gecko)
300px
9A33BM transporter erector launcher and radar (TELAR)
Type 6x6 amphibious SAM system
Place of origin Soviet Union
Service history
In service 1971-present
Used by See list of present and former operator
Wars 1982 Lebanon War, Angolan Civil War, Persian Gulf War, 2008 South Ossetia war, 2011 Libyan civil war
Production history
Designer NII-20 Research Institute
Designed 1960-1972
Manufacturer Znamya Truda Plant
Produced 1970-1988[1]
Number built 1200[2]
Variants OSA-A, OSA-AK, OSA-AKM, OSA-M
Specifications (OSA-AKM)
Weight 17.5 tonnes
Length 9.14 m
Width 2.75 m
Height 4.20 m (radar mast stowed)
Crew 5 soldiers

Main
armament
6 9M33, 9M33M1, 9M33M2 or 9M33M3 missiles
Engine D20K300 diesel
Ground clearance 400 mm
Operational
range
500 km
Speed 80 km/h
8 km/h (swimming)

The 9K33 Osa (English: wasp) is a highly mobile, low-altitude, short-range tactical surface-to-air missile system. "9K33" is its GRAU designation. Its NATO reporting name is SA-8 Gecko. Its export version name is Romb.[3]

Description

The SA-8 was the first mobile air defense missile system incorporating its own engagement radars on a single vehicle.

All versions of the 9K33 feature all-in-one 9A33 transporter erector launcher and radar (TELAR) vehicles which can detect, track and engage aircraft independently or with the aid of regimental surveillance radars. The six-wheeled transport vehicles BAZ-5937 are fully amphibious and air transportable. The road range is about 500 km.

The 1S51M3-2 radar system on the SA-8 TELAR received the NATO codename Land Roll. It was derived from the naval `Pop Group' radar system but is smaller since it does not require the elaborate stabilisation system. An improved system designated the SA-8B `Gecko' Mod 1, was first seen in Germany in 1980. It had improvements added to the launcher configuration, carrying six missiles in ribbed containers. The system is reported to be of the frequency-agile monopulse type. It consists of an elliptical rotating surveillance antenna mounted on top of the array, operates in H band (6 to 8 GHz) and has a 30 km acquisition range against most targets. The large pulsed J band (14.5 GHz) engagement antenna is mounted below it in the centre of the array and has a maximum tracking range of about 20 km.

Mounted on either side of the tracking radar antenna is a small J band parabolic dish antenna to track the missile. Below that is a small circular antenna which emits an I band uplink capture beam to gather the missile shortly after launch. The final antennas in the array are two small white rectangular ones, one on either side of the array mounted alongside the I band. These are used for command uplink to the missile. This twin antenna system permits the 'Land Roll' radar to control up to two missiles simultaneously against a single target. Furthermore, the two missiles can be guided on different frequencies to further complicate ECM. There is also a tubular device fitted to and above the tracking radar; this is a 9Sh33 electro-optical tracker. It can be used to track the target when the main tracking radar is jammed by ECM.

A 9K33 battery comprises four 9A33B TELAR vehicles and two 9T217 transloader vehicles on BAZ-5939 chassis with reload missiles and a crane. A reload time of five minutes has been reported per TELAR.

In addition to the TELARs, each regiment is also assigned a single radar collimation vehicle 9V914 (initially on the BAZ-5938 chassis but more often found on the ZiL-131 truck). This vehicle assists in the alignment of the TELAR's radar systems, ensuring accurate target tracking and engagement.

Variants

File:SA-N-4.jpg
SA-N-4 launcher covered by a circular plate on the Slava class cruiser Marshal Ustinov.
  • 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).
  • 4K33 "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.
  • Saman and Saman-M (Russian Саман – adobe) is a development of the Osa\Osa-M system into target drones, used for testing and training with air defense systems, including SAMs.

The 9K33M3 is also able[citation needed] to utilize the 9A33BM3 missiles which are wire-guided, presumably for use in an ECM-heavy environment where the radio command guidance may not operate properly.

Missiles

9M33
300px
The 9M33M3 missile
Type Surface-to-air missile
Place of origin Soviet Union
Service history
In service 1971-present
Used by See list of present and former operator
Production history
Designer MKB "Fakel"
Designed 1960-1972
Manufacturer Znamya Truda Plant
Produced 1970-1988
Variants 9M33, 9M33M1, 9M33M2, 9M33M3, 9A33BM3
Specifications (9K33M3[4])
Weight 170 kg
Length 3158 mm
Diameter 209.6 mm
Warhead Frag-HE
Detonation
mechanism
Contact and proximity

Propellant Solid propellant rocket motor
Operational
range
15 kilometres (9.3 mi)
Flight altitude 12,000 metres (39,000 ft)
Boost time 2 s boost, then 15 s sustain
Speed 1020 m/s
Guidance
system
RF CLOS
Steering
system
dual-thrust rocket motor.
Accuracy 5 m
Launch
platform
9P35M2

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.

There have been unconfirmed reports of other possible versions of the missile with both infra-red and semi-active radar terminal homing seekers.

Each TELAR is able to launch and guide two missiles against one target simultaneously. Kill probability is quoted as being 0.35-0.85 for the Osa and 0.55-0.85 for the Osa-AK and Osa-AKM (presumably depending upon target aspect, speed, maneuverability and radar cross section). Reaction time (from target detection to launch) is around 26 seconds. Time to prepare for engagements from being in transit is around 4 minutes and missile reloading takes around 5 minutes. Each battery of four TELARs is usually accompanied by two reload vehicles carrying 18 missiles in sets of three, with a crane mounted on the reload vehicles to assist in moving the missiles.

When launched the booster motor burns for two seconds, this permits the radar to gather and control it at very short ranges (about 1.6 km). The sustainer motor has a 15-second burn, bringing the missile to a top speed of about Mach 2. Once launched the missile is command-guided for the whole flight, and the warhead is detonated by its proximity fuze or possible command. The warhead is said to have a lethal radius of 5 m at low altitude against a F-4 Phantom size target.[citation needed]

Radars

File:Longtrack.jpg
P-40 'Long Track' radar set
  • 1S51M3 ("Land Roll") - C band target acquisition radar, H band conical scan target tracking radar and two J band pulse mode fire control radars (range 35 km/22 miles for acquisition, 30 km/19 miles for tracking and 25 km/16 miles for guidance). Mounted on the TELAR.
  • P-40 ("Long Track") - E band early warning radar (also used by the SA-4 and SA-6, range 175 km/108 miles), mounted on a tracked vehicle (a modified AT-T).
  • P-15 ("Flat Face A") or P-19 ("Flat Face B") or P-15M(2) ("Squat Eye") - 380 kW C band target acquisition radar (also used by the SA-3 and SA-6, range 250 km/155 miles), mounted on a ZiL-131 truck.
  • PRV-9 or PRV-16 ("Thin Skin") - E band height finding radar (also used by the SA-4 and SA-6, range 240 km/148 miles), mounted on a KrAZ-255B truck.

Deployment and History

As well as the USSR/Russia, there are many export customers for this system, including Cuba, Greece (from the former East Germany), Poland, Syria, Ecuador and Iraq. In late 80's Cuba deployed several SA-8 units in southern Angola and posed a significant threat to South African air superiority at shorter ranges.[5] Iraq used Osa systems during the 1991 Gulf War. South African 61 Mechanised Battalion Group captured a complete SA-8 anti-aircraft missile system on 3 October 1987 during the Battle of Cuito Cuanavale. This was the first time that such a system had ever fallen into non-Warsaw Pact forces hands, giving Western intelligence agencies an opportunity to examine an important Soviet-bloc weapon system.[6] The system was also seen used in the 2008 South Ossetia War by both Georgians and Russians. Libyan SA-8s were used and some destroyed during the 2011 Libyan war.[7][8]

Syrian Civil War

During the Syrian civil war in December 2012, rebels fighting Bashar al-Assad's forces managed to capture at least one Osa system after a raid on an air defense base near Damascus.[9] Later, on different occasions, videos showing rebels using the system appeared. On 31 July 2013, a video surfaced showing the successful missile launch for a rebel operated Osa system with a possible hit on a Syrian helicopter.[10] On 16 January 2014 a video of the shooting down of a Syrian Mi-8 or Mi-17 helicopter was uploaded. The heavy damage on the plunging helicopter appeared to confirm the use of a bigger missile to hit the helicopter compared to the damage caused by MANPADS. Also, a video filming the TV screen inside the Osa vehicle matches another video taken outside. Another video surfaced on 18 January 2014, this time missing the intended target.[11] On 15 October 2015 Russian military reported that a 9K33 Osa Launcher captured by rebel forces was destroyed in an air strike by a Russian Su-34 bomber near Damascus.[12]

Command post

PPRU-M1 (PPRU-M1-2) is a mobile command center for a mixed grouping of air defense forces, such as 9K33 Osa and SA-15 Gauntlet, 9K22 Tunguska, SA-13 Gopher, 9K38 Igla[13]

Upgrades

Belarus

  • The 9K33-1T "Osa-1T" was developed by UE "Tetraedr" from Belarus. A SAM system comprises combat assets and technical support means, including
    • the 9А33-1Т TELAR or "Combat Vehicle" (CV), based on the original BAZ-5937 (or the new MZKT-69222) and equipped with a new day/night camera system OES-1T instead of the original day-only 9Sh33 or 9Sh38-2 "Karat";
    • the 9M33M2 or -3 SAMs, or the new 9M33M3-1 with a range of 20 km;
    • the 9Т217-1T Transportation and Loading Vehicle (TLV);
    • the 9V210-1T Maintenance Vehicle (MV);
    • the 9V214-1T Alignment Vehicle (AV);
    • the 9V242-1T Automatic Mobile Check-up and Testing Station (AKIPS) and
    • the 9F16M2 Ground Equipment Kit (GEK).[14][15][16]
  • The T38 "Stilet" is a further development of the Osa-1T. Main components are the TELAR T381 on MZKT-69222 chassis and the new missile T382. Maximum range of targets’ destruction 20 km, minimal RCS of targets detected 0.03 m².[17]

Poland

  • Osa-AKM-P1 "Żądło" (export name SA-8P Sting) is a Polish upgrade of the 9K33M2 "Osa-AK" and 9K33M3 "Osa-AKM". Probably 32 of the 64 systems purchased from the Soviet Union will be upgraded to keep them in service until 2017. An upgraded TELAR 9A33BM3-P1 was displayed at the MSPO 2004 exhibition in Kielce, Poland. The upgraded vehicle is fitted with a passive detection and identification system SIC 12/TA as well as the ISZ-01 IFF system.[18][19][20]

Operators

Map of 9K33 operators in blue with former operators in red
File:Romanian SA-8.jpg
Romanian 9K33 Osa missile launch at Capu Midia firing range.

Current operators

Former Operators

References

External links

Notes

  1. http://www.kupol.ru/company/history
  2. http://www.raspletin.ru/zenitnyy-raketnyy-kompleks-osa
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  5. George, Edward in: The Cuban Intervention in Angola, 1965-1991, Frank Cass, London, New York, 2005, ISBN 0-415-35015-8, p. 236-237
  6. Turton, A.R. 2010. Shaking Hands with Billy. Durban: Just Done Publications.
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  9. SYRIAN REBELS CAPTURE MOBILE ROCKET LAUNCHER; During attacks [GunFire + Chanting] on YouTube
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  15. http://www.tetraedr.com/mupload/iblock/d52/d521887e3fe536d84c3440378450e0c0.pdf
  16. http://www.tetraedr.com/mupload/iblock/588/58800b30e603bcc2b990aa5091daa7a5.pdf
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  22. The Military Balance 2010. — P. 245. +The Military Balance 2012. — P. 317.
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