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Type 81 Tan-SAM


81式短距離地対空誘導弾


Overview


Type 81 Tan-SAM

Launch vehicle of the Type 81 Tan-SAM system seen on the move in 2017.
Source: Hunini - © CC BY-SA 4.0

Origin
Japan
Type
Self-propelled SAM system
Entered service
1982
Status
In service
Development
1966 - 1978 (Tan-SAM)
1989 - 1995 (Tan-SAM kai)
Developer
Japan - Toshiba
Production
1981 - 1990's (systems)
1980 - present? (missiles)
Producer
Japan - Toshiba
Number produced
Over 100 launch vehicles
About 1.800 missiles
Designations
81式短距離地対空誘導弾
Type 81
短SAM / Tan-SAM
Notable users
Japan

Description


Introduction

The Type 81 Tan-SAM is a surface to air missile of Japanese origin. It was developed for the Japanese armed forced to fill the gap between the man-portable Stinger and fixed position Hawk missiles. The name Tan-SAM stands for "short-range surface to air missile".

Design

The Tan-SAM system consists of a fire control vehicle equipped with radar and two launch vehicles. The launch vehicles can have up to four missiles ready to launch but are often seen with just two. The total crew of a Tan-SAM system totals 15. All vehicles are based on the Type 73 6x6 truck and are unarmored.

Fire control

The radar vehicle is used to detect the targets and to provide data for the missiles. Upon launch the missiles are fired in the direction of the target and after an inertial flight pattern the missile acquires the target and intercepts it. The original Tan-SAM missile has an infrared seeker and the newest model uses an active radar seeker. Each launcher has an optical director that allows the missiles to be fired without fire control information.

Firepower

The Tan-SAM has a maximum range of 10 km and maximum altitude of 3 km. The original missiles feature a high quality infrared seeker with limited protection against decoys. The latest missiles feature an active radar seeker which is less prone to jamming and extends the maximum range to 14 km.

Mobility

The Type 81 Tan-SAM missile system is based on Type 73 6x6 trucks. This makes the system very mobile on roads, with the mobility in the field being limited. The system is not able to fire on the move and takes about 30 minutes to set up.

Users

The sole operator of the Type 81 is Japan. It was adopted by all three branches of the military. Over recent years several improvement programs have been carried out, resulting in the improved Tan-SAM kai. The Tan-SAM is not offered for export.

System composition


Type 81 launch vehicle

The Type 81 launch vehicle is based on the Isuzu Type 73 6x6 truck. The launcher has two arms on which two missiles can be attached, one on top and one below. A datalink provides the missile with information given by the fire control vehicle before launch. Reloading the missiles takes about 3 minutes.

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.

Type 81 missile

The Tan-SAM is a conventional missile with cruciform wings in the middle and at the rear. Unlike most vehicle launched systems it uses an infrared seeker, which is more common on shoulder launched missiles. Inertial navigation is used to extend the effective range beyond the range of the infrared seeker.

Tan-SAM-1: Original missile with infrared seeker.
Tan-SAM-1B: Similar to Tan-SAM-1 but has an improved infrared seeker.
Tan-SAM-1C: Missile used Tan-SAM Kai upgrade which has an improved rocket motor and uses a phased array active radar seeker.

Details


Facts Tan-SAM Tan-SAM kai
General
Origin
Japan
Type
Surface to air missile
Dimensions
Length
2.7 m
Diameter
0.16 m
Wingspan
0.6 m
Weight
100 kg
Guidance
Terminal phase
Passive infrared homing
Initial phase
Pre-programmed autopilot
Warhead
Type
HE-Fragmentation
Weight
9.2 kg
Fuse
Contact and radar proximity fuses
Engagement envelope
Propulsion
Single-stage solid propellant rocket motor
Speed
Mach 2.4
Range
10 km maximum
7 km effective
0.5 km minimum
Altitude
3 km effective
15 m minimum

Media


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