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Military Equipment Database
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M26

M26

Rockets
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Basic Information
Name
M26
Designation
M26
Alternate Designation
Equipment Type
Rockets
Manufacturer
Date of Introduction
Description

The M26 rockets are spin-stabilized unguided projectiles. They are powered by a solid fuel rocket motor. Once fired, the M26 rocket follows a ballistic trajectory. The M26 rockets are stored in individual tubes which provide storage and act as the launch ramp. The 2 launch containers employed by the M270 MLRS rocket artillery system consist of 12 (2x6) M26 rockets inside their associated tubes. The M26 rocket is the main ammunition of the M270 MLRS (Multiple Launch Rocket System). Both were combat proven successfully in 1991, during the operation Desert Storm. The M28 is a training rocket designed to simulate the M26 rocket firing. The M26 rocket has been fielded in 14 countries around the world. Each M26 rocket carries up to dual purpose 644 M77 DPICM submunitions detonated by impact at a maximum range of 32 km. Employing the M77 submunitions a M26 rocket can cover an area of 0.23 square kilometers.

Overview (Deagel)
Group Rockets
Status Retired - No Longer Operational
Also Known As M28 (training rocket), M28A2
Origin United States of America
Contractor Lockheed Martin
Initial Operational Capability (IOC) 1989
Total Production ?
Specifications (Deagel)
Number of Submunitions 644
Dimensions — Caliber 227 millimeter
Dimensions — Length 3.9 meter
Mass — Weight 306 kilogram
Performance — Max Range 32,000 meter
Performance — Min Range 11,500 meter
Gear (Deagel)
Item 1 Rockets: Corect (1)
Variants
Variant 1 M26
Variant 2 M26A1
Details
Country of Origin United States
Classification
Domain
Ground
Equipment Status
Active
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