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Surface-to-Air Missiles ยทToshiba

Missile SAM-1

Japanese surface-to-air missile, entering service in 1981, utilizes a phased array active radar seeker. Key figures: range 40 km, top speed 2,400 km/h, warhead 9 kg, guidance Phased array active radar seeker, in service since 1981. In service with 1 country โ€” Japan.

Range
40km
Max speed
2,400km/h
Produced
107units
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 1.9)
SAM-1 scale diagram
SAM-1 โ€” Surface-to-Air 1.75 m 2.70 m
Range
40 km
Speed
Mach 1.9
Weight
100 kg
Warhead
9 kg
Operators
๐Ÿ‡ฏ๐Ÿ‡ต 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.

Wikipedia (CC BY-SA) and other open sources. Last updated on 25 January 2026. Suggest a change

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.
Compare This Missile
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Latest Data Updates
  1. JAN 252026 Updated Range and max speed updated
  2. JAN 192026 Updated Description, span and 6 more fields added
  3. JAN 182026 Updated Sources and cross-references refreshed