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Type 81 Tan Japanese Surface to Air Missile (SAM) System

Type 81 Tan-SAM Kai

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Basic Information
Name
Type 81 Tan Japanese Surface to Air Missile (SAM) System
Designation
Type 81 Tan-SAM Kai
Alternate Designation
Type 81 Tan-SAM Kai
Equipment Type
Manufacturer
Toshiba
Date of Introduction
1981
Description

The Type 81 Tan Japanese Surface to Air Missile System Missile (SAM) was developed and deployed with the Japanese Self Defense Force (JSDF) to fill a gap between the US made Stinger (initially) and later the Toshiba Type 91 MANPADS and the fixed based Hawk missiles. "Tan" translates to short as in short range. The system provides a defense ring against manned and unmanned aerial platforms that are able to penetrate through forward interceptor and area defense systems. Prior to operation, each launch vehicle and the fire control vehicle is leveled and stabilized by their respective hydraulically operated jacks. Electrical cables are employed to connect the telephone/data link system with each vehicle. Generally, the fire control vehicle is located about 300 meters from the two launchers. The time of preparation is approximately 30 minutes. The missile is designed and produced as a blunt top cylinder configuration along with cruciform cropped delta wings in the middle and moveable cruciform tail wings. Two infrared red seeker covers capable of rotating 180 degrees protect the missile heads during transit. The launcher is powered by a 30kW generator when the vehicle engine is turned off. The fire control system computer pre-programs the scanning angle of the seeker head prior to launch to prevent the missile from tracking the sun as well controlling the launcher assembly to prevent an accidental launch directly at the sun. Once fired the seeker is activated and the seeker head scans the preprogrammed area of the sky to find the target. The the guidance unit locks onto the target and the missile travels the shortest course to intercept the target. The lethal radius of the missile is 5 meters to 15 meters depending on the type of target. There is no self destruct capability. The Tan SAM Kai is the product improved version of the Type 81. It has an improved smokeless rocket motor and uses a phased array active radar seeker. Toshiba, Tokyo, Japan is the prime contractor with the following industries as subcontractors: Nissan Motor, Aerospace Division (rocket motor) Fuji Heavy Industries (launcher assembly less electronics) Isuzu Motors (Type 73 Truck) Kawasaki Heavy Industries (autopilot and missile body) It is not available for export.

Ground Specifications
Crew 2
Mobility Type Wheeled (6x6)
Main Weapon Tan SAM Kai missile on a quadruple launcher with 4 missiles ready to fire
Max Speed 2962.6 km/h
Range 500.0 km
Variants
Type 81 Fire Control Vehicle The Type 81 fire control vehicle is able to control two launch vehicle. It is based on the same Type 73 6x6 truck as the launch vehicle. A generator powers the fire control equipment and the roof mounted phased array radar, which has a 30 km range. In the Tan-SAM kai upgrade the fire control vehicle is also able to relay mid course updates to the active radar homing missiles.
System
Alternative Designation Type 81 Tan-SAM Kai
System The Type 81 System consists of 2 each launcher vehicles, a fire control vehicle equipped with the radar, and other support vehicles.
Manufacturer Toshiba
Configuration 6x6
Crew 2 (driver and assistant) launcher; 4 ((commander, radar operator, 2 launcher operators) Fire Control Unit. 3 for the Support Vehicles :Total System 15
Automotive
Vehicle Type Type 73 6x6 chassis
Length 6.89 m
Width 2.43 m
Height INA m
Weight 3,054 kg
Wheelbase 3.26 + 1.19 m
Engine Model 8PC1 V6 diesel, 210 hp ag 2,200 rpm
Transmission Manual, 5 forward, 1 reverse
Speed 90 on road km/h
Fuel Capacity 140 L
Range 500 km
Fording 0.8 m
Armament
Primary Weapon
Launcher Name Type 81
Launcher Type Tan SAM Kai missile on a quadruple launcher with 4 missiles ready to fire.
Traverse 360 deg, powered non-stabilized
Fire on Move No
Reaction Time INA
Reload Time 3 min estimated for 4 missiles
Time between Launches INA
System Emplacement Time 30 min
System Displacement Time INA
Munition
Type 81 Tan Surface to Air Missile (Kai Upgrade)
Name Type 81
Diameter (Body) 0.16 m
Wingspan 0.6 m
Length 2.7 m
Weight 100 kg
Fuze Type Contact and radar proximity fuses
Type Warhead Frag-HE 9.2kg
Guidance Pre-programmed autopilot with passive infrared terminal homing
Probability of Hit 75 PCT
Propulsion Single stage solid fuel propellent rocket motor
Range, Maximum 14,000 m
Range, Minimum 500 m
Altitude, Maximum 3,000 m
Altitude, Minimum 15 m
Seeker Field of View INA
Self-Destruct Time INA
Target Maneuver Limit INA
Speed Mach 2.4
Tracking Rate INA
Basic Load 4 ea
Fire Control System
ADAD INA
IFF Yes
Target Alert Display Set (TADDS) INA
Day Sight
Acquisition Range INA km
Field of View INA deg
Field of View INA deg
Type INA
Night Sight
Type INA
Night Sights
Acquisition Range INA km
Field of View INA deg
Radar
Radar Equipment 3D Phased Array pulse doppler radar with a range of 30km, 360 degrees coverage, and IFF system.
Radar Other Mounted on a separate radar vehicle. The Type 81 kai upgrade includes the radar's ability to relay mid course updates to the active radar homing missiles.
Details
Country of Origin Japan
Filter Label
T
Classification
Domain
Ground
Equipment Status
Active
Dimensions
Length
6.89 m
Width
0.16 m
Height
Weight
3054 kg
Operators (1)
Japan
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