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Type 87 Chu-MAT
Photo: No machine-readable author provided. Los688 assumed (based on copyright claims). · Wikimedia Commons · Public domain
REC // INTEL FEED

Type87Chu-MAT

Anti-Tank Guided Missiles (ATGM) · Japan · 1989
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Type87Chu-MAT

Type 87 Chu-MAT
Type 87 Chu-MAT Photo: No machine-readable author provided. Los688 assumed (based on copyright claims). · Wikimedia Commons · Public domain
* Absolute score — assessed within category · no era adjustment
Penetration
65
Range
60
Guidance / Accuracy
70
Fire-and-Forget
0
Top-Attack Capability
0
Portability
75
Counter-Measure Resistance
50
Reliability
70
Technology
60
Cost-Effectiveness
80
Origin Japan
ManufacturerKawasaki Heavy Industries
CategoryAnti-Tank Guided Missiles (ATGM)
EraCold War
In service1989–2027
Operators1 countries
Data Quality82%
51
Anti-Tank Guided Missiles (ATGM) MASS Rating
17/35
Cold War
52/86
All-Time
Anti-Tank Guided Missiles (ATGM) · 10 axes scored
Penetration
65
Range
60
Guidance / Accuracy
70
Fire-and-Forget
0
Top-Attack Capability
0
Portability
75
Counter-Measure Resistance
50
Reliability
70
Technology
60
Cost-Effectiveness
80
ⓘ Regardless of era, the same scoring system applies to all units in the anti-tank guided missiles (atgm) category.
01 / Overview
Type 87 Chu-MAT
Country
Production
1989–2027
Operators
💰 PERFORMANCE / PRICE ASSESSMENT Methodology ↗
ANTI-TANK GUIDED MISSILES (ATGM) · COLD WAR
17
PERFORMANCE/PRICE
76
UNIT COST (2025 USD)
—
51
anti-tank guided missiles (atgm) category
ⓘ Performance/Price and MASS score are computed across all units in the anti-tank guided missiles (atgm) category, regardless of era.
02 / Specs & Design
◎General7MOD.7
  • Missile TypeAnti-Tank Guided Missile
  • Service Entry Year1989
  • DesignerDefense Agency Technical Research and Development Institute
  • Length1 m
  • Diameter110 mm
  • Launch Weight12 kg
  • In ServiceYes
▣Propulsion5MOD.5
  • Propulsion Typesolid-fuel rocket
  • Motor Typesolid-propellant rocket motor
  • Boost StageYes
  • Two-StageNo
  • Fuel / Propellantsolid propellant
◇Performance3MOD.3
  • Maximum Range2 km
  • Flight Profileline-of-sight, command-to-line-of-sight
  • HypersonicNo
◆Warhead4MOD.4
▤Launch Platform6MOD.6
⬢Production3MOD.3
  • Operators1
  • Variants0
  • Production Start1,987 year
▲Warhead Detail2MOD.2
  • Detonation Mechanism / Fuzecontact fuze
  • Explosive Filler TypeHEAT
03 / History
SERVICE LIFESPANStill in Service
  1. 1989Production started
  2. 2027Production ended
37
years in service
38
years in production
1
countries operating
ⓘ The producing country still actively operates it.
04 / Operators
Operator Countries1country
📖 TERMS ON THIS PAGE3terms
The initial propulsion phase where a high-thrust motor accelerates the missile to operational velocity.
Launched from a ground-based platform, such as a vehicle or tripod, rather than an aircraft or other airborne system.
A guidance system that uses directed laser beams to track and adjust the trajectory of a missile toward its target.
These terms are listed automatically because they appear on this page.full encyclopedia →
📚 Sources
📖 ENCYCLOPEDIA Browse the Anti-Tank Guided Missiles (ATGM) entry →