Missile SAM-1

Summary

CategorySurface-to-Air Missiles
Sub-typeRadar-guided surface-to-air missile
Origin country 🇯🇵 Japan
ManufacturerToshiba
StatusIn service
Year of service1981
Number built107 units

Technical specifications

WarheadHigh Explosive
Warhead weight9 kg (20 lb)
Diameter160 mm (6.3 in)
Span600 mm (23.6 in)
Length2,700 mm (106.3 in)
Flight altitude3,000 m (9,843 ft)
Weight100 kg (220 lb)
Range 40 km (25 mi)
Max. speed2,400 km/h (Mach 2.4)

SAM-1 scale diagram

SAM-1 — Surface-to-Air 1.75 m 2.70 m
Range
40 km
Speed
Mach 2.4
Weight
100 kg
Warhead
9 kg

Operators

🇯🇵 Japan

Description

Development of the system commenced in 1966 to replace the 75 mm M51 Skysweeper and M15A1 anti-aircraft guns. The project was intended to fill the performance gap between man-portable missiles and larger-scale surface-to-air systems. Test firings were conducted in 1978, and the system entered service in 1981. A minor variant, designated SAM-1B, was introduced in 1987. An upgrade program for the SAM-1C began in 1989, with production starting in 1996. Research results from the subsequent Kai II program were later incorporated into the Type 11 system.

The missile is propelled by a single-stage solid-fuel rocket motor; the SAM-1C variant utilizes an improved smokeless motor. Initial flight is governed by inertial guidance to a predicted intercept point. Terminal guidance is provided by an all-aspect passive infrared seeker, while the SAM-1C variant utilizes a phased array active radar seeker and can receive mid-course guidance updates. The missile is equipped with a fragmentation warhead featuring both contact and radar proximity detonation mechanisms. The airframe is configured with four mid-body clipped delta wings and four steerable rear fins.

A standard fire unit comprises a Fire Control System (FCS) vehicle and two launcher vehicles mounted on 6x6 trucks. The FCS vehicle employs a three-dimensional pulse-doppler phased array radar with three operating modes: omni-directional search, sector search, and fine tracking. The radar can track multiple targets simultaneously and includes integrated Identification Friend or Foe (IFF) capabilities. Launchers can be positioned at a distance from the FCS vehicle to increase survivability. For operation in electronic countermeasure environments, the system includes an optical director, and the SAM-1C variant is equipped with a thermal imager. Each launcher is also fitted with heavy machine guns for self-defense against ground threats and close-in aerial targets.

The system is currently in service with the Japan Ground Self-Defense Force, the Japan Air Self-Defense Force, and the Japan Maritime Self-Defense Force. It is widely deployed across these branches as a mobile short-range air defense asset.

Frequently Asked Questions

What type of missile is the SAM-1?
The SAM-1 is a surface-to-air missile developed by Japan. It entered service in 1981.
What is the range of the SAM-1?
The SAM-1 has a maximum range of approximately 40 km (24 miles). Effective range varies with launch platform, altitude, and flight profile.
How fast is the SAM-1?
The SAM-1 reaches a maximum speed of 2,400 km/h (Mach 1.9).
What warhead does the SAM-1 carry?
The SAM-1 carries a high explosive warhead weighing 9 kg.
How is the SAM-1 guided?
The SAM-1 uses phased array active radar seeker guidance.
Which countries use the SAM-1?
The SAM-1 is in service with 1 country: Japan.
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