9K33 Osa

The Polish OSA-AKM

Osa 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-launcherand radar 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 9K33 Osa 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, the Osa-AKM (NATO reporting name 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.

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 to use the 9A33BM3 missiles which are wire-guided, presumably for use in an ECM-heavy environment where the radio command guidance may not operate properly.

9M33
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[5])
Mass	170 kg
Length	3158 mm
Diameter	209.6 mm
Warhead	Frag-HE
Warhead weight	16 kg[6]
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
Maximum 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 50–5,000 m (164–16,400 ft). The 9M33M2 "Osa-A" missile extends the ranges out to 1,500–10,000m (1–6.2 miles) and engagement altitudes to 25–5,000 m (82–16,400 ft). The 9M33M3 missile greatly enhances the altitude engagement envelope to 10–12,000 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.

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 2K11 Krug and 2K12 Kub, 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 S-125 Neva and 2K12 Kub, 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 2K11 Krug and 2K12 Kub, range 240 km/148 miles), mounted on a KrAZ-255B truck.

Produced by the USSR/Russia, there are many export customers for this system, including Cuba, Greece (from the former East Germany), Poland, Syria, Ecuador and Iraq.

After the Israeli invasion of Lebanon in 1982, in which Syrian air defenses were oblitarated by a massive air campaign against Syrian SAM sites in the Beqaa valley, the Syrians managed to deploy SA-8s. At least one F-4 Phantom in a SEAD mission was shot down on July 24, 1982 by an SA-8 system. The WSO (back seater), Aharon Katz was killed, while the pilot, Gil Fogel, survived and was held captive by the Syrians for two years.[7]

In late 1980s, Cuba deployed several 9K33 Osa units in southern Angola which posed a significant threat to South African air superiority at shorter ranges.[8] The South African 61 Mechanised Battalion Group captured an intact 9K33 Osa 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 the hands of non-Warsaw Pact forces, giving Western intelligence agencies an opportunity to examine an important Soviet-bloc weapon system.[9]

Iraq used Osa systems during the 1991 Gulf War.

The system also saw use in the 2008 Russo-Georgian War by both the Georgian and Russian militaries.

Libyan 9K33 Osa were used, and some destroyed during the 2011 Libyan Civil War by NATO airstrikes.[10][11] In order to prevent the threat to Azerbaijani aerial vehicles and suppress the enemy's activism, Azerbaijani Armed Forces have destroyed OSA surface-to-air missile system, a re-supply vehicle and personnel of the Armenian Armed Forces on 15 May 2017.[12]

PPRU-M1 (PPRU-M1-2) is a mobile command center for a mixed grouping of air defense forces, such as 9K33 Osa and Tor missile system, 9K22 Tunguska, 9K35 Strela-10, 9K38 Igla[23]

Wikimedia Commons has media related to 9K33 Osa.

• Federation of American Scientists page
• Astronautix.com
• ROSOBORONEXPORT

• AIR-DEFENCE MISSILE LAUNCHER 9K33 "OSA"( 9A33 -CARRIER, 9M33 – MISSILES)(SA-8 GECKO) – Walk around photos
• SA-8 Gecko 9K33 OSA Ground-to-air missile system
• 9K33M2 OSA-AK (SA-8B Gecko) Simulator