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9M83


NATO: SA-12A / SA-23A Gladiator


Overview


9M83ME in launch canister

A launch canister of a 9M83ME (NATO: SA-23A Gladiator) missile on display at an airshow in Russia in 2011.
Source: Vitaly V. Kuzmin - © CC BY-SA 4.0

Origin
Soviet Union
Type
Surface to air missile
Entered service
1983
Status
In service
Development
1970's
Developer
Soviet Union - OKB-8 Novator
Production
Early 1980's - present
Producer
Soviet Union
Russia
Designations
SA-12A Gladiator (NATO reporting name for 9M83)
SA-23A Gladiator (NATO reporting name for 9M83M)

Description


Introduction

The 9M83 is a late Cold War era surface to air missile of Soviet origin. It is a high performance missile used with the S-300V surface to air missile system. The 9M83 is the smaller of the two missile sizes used with the S-300V and is known in the West as the SA-12A Gladiator.

Design

The 9M83 is a surface to air missile of a rather unique design. It is a high speed two stage missile using thrust vectoring. The missile is carried and launched in its transport container. Upon launch a gas generator propels the missile from the launch tube. While suspended in the air the main engine kicks in and four vanes within the nozzle steer the missile in the target's direction. The second stage of the missile has eight tailfins and houses the homing system and warhead in the nose.

Guidance

The 9M83 uses inertial navigation upon launch. The launch vehicle can also provide mid course updates via datalink. Once the missile reaches the target airspace the semi-active radar homing head is activated. The target is illuminated by the fire control radar on the launch vehicle. In case of the 9M83 missile the radar on the launch vehicle is located on a mast for optimal illumination of low flying targets. A radio command fuse sets off the warhead.

Firepower

The 9M83 has a maximum effective range of 75 km against aircraft and 40 km against missiles. Since the illumination radar is mast mounted the minimum target altitude can as little as 25 m. Maximum altitude is quoted as 25 km. The 9M83 is a two stage missile with maximum flight speeds of 1.200 m/s and 1.700 m/s respectively. As with all air defense missiles effective range and speed are highly dependent on target parameters and chosen flight path for interception.

Launch platforms

The 9M83 is used with the S-300V and S-300VM surface to air missile systems. The S-300V is built to keep up with army formations and is based on large tracked vehicles. The launch vehicles and transloaders both have four missiles ready to launch. The launch vehicle has a mast mounted target illumination radar while the transloader is fitted with a crane. Unlike many other Soviet surface to air missiles there is no naval equivalent using this missile.

Users

The S-300V was acquired by the Soviet Union to accompany and protect larger army formations. The S-300V was introduced in 1983 and at first only had the 9M83 missile ready for launch, before the larger 9M82 became operational in 1988. S-300V was only in service with the Soviet Union and ended up in Russia and Ukraine. S-300VM was also acquired by Egypt and Venezuela.

Variants


9M83

A 9M83 series surface to air missile on public display.
Source: Unknown author - © Copyright lies with original owner

Variants of the 9M83

9M83
Medium range missile used in the 9K81 / S-300V system. NATO reporting name is SA-12A Gladiator. Maximum range is 75 km.
9M83M
Improved model used with 9K81M / S-300VM system. It has a longer range and higher speed. Maximum range is quoted as 90 to 100 km depending on source. This is achieved by reducing size and weight of electronics in exchange for more fuel. NATO reporting name is SA-23A Gladiator.
9M83ME
Export model of the 9M83M.
9M83MD
Longer range variant of the 9M83M. Unknown whether this is a proposed design, a prototype or actually in production. Claimed range of 120 to 150 km depending on sources.

Details


Facts 9M83
General
Origin
Soviet Union
Type
Surface to air missile
Dimensions
Length
7.90 m
Diameter
0.915 m
Wingspan
1.213 m
Weight
2.290 kg
1.077 kg first stage
1.213 kg second stage
Guidance
Terminal phase
Semi-active radar homing
Initial phase
Inertial only
Inertial with mid course update via datalink
Warhead
Type
9N127 high explosive fragmentation
60° fragment cone
Weight
150 kg
Fuse
9E322 radio command
Engagement envelope
Propulsion
Solid fuel rocket motor in each stage
Speed
1.200 m/s first stage
1.700 m/s second stage
Range
75 km maximum
40 km against missiles
6 km minimum
Altitude
25 km maximum
0.025 km minimum
G force
20 G

Media


Related articles


9M82

The 9M82 is the long range counterpart intended for use against ballistic missiles. It has a much larger boost section doubling the total weight of the missile.

S-300V

The 9M83 missile is used with the S-300V surface to air missile system.