Naze'at 6-H Iranian Close-Range Ballistic Missile
Naze'at 6-H , Naze'at 6
Surface to Surface Ballistic Missile / Long-Range Artillery Rocket
Other
Basic Information
Name
Naze'at 6-H Iranian Close-Range Ballistic Missile
Designation
Naze'at 6-H , Naze'at 6
Alternate Designation
Naze'at 6-H , Naze'at 6
Equipment Type
Surface to Surface Ballistic Missile / Long-Range Artillery Rocket
Manufacturer
—
Date of Introduction
1981
Description
Hezbollah Proliferation. The Naze'at 6-H is an Iranian close-range ballistic missile (some classify it as rocket artillery) with a range of about 100 km. Like Iran's similarly shaped Zelzal rockets, Naze'at rockets do not have a guidance system. The Naze'at 6-H is also widely known without the -H suffix, as the Naze'at 6. The Naze'at is launched from a transporter erector launcher (TEL) and carries a conventional warhead. It may be capable of carrying a chemical or biological warhead as well. A complete Naze'at system includes a TEL and communications vans, meteorological vans, and a GPS system for surveying the launch site. The reliability and accuracy of Naze'at rockets is assessed as poor as they have no guidance system.
Air & Air Defense Specifications
Max Speed
4939.2 km/h
Range
100.0 km
Variants
Naze'at 10-H
Improved version with a longer range rocket.
System
Alternative Designation
Naze'at 6-H , Naze'at 6
Date of Introduction
1980
Proliferation
Hezbollah
Type
Surface to Surface Ballistic Missile / Long-Range Artillery Rocket
Family
Naze'at
Crew
INA
Chassis
INA
Displacement Time
INA
Emplacement Time
INA
Dimensions (Chassis)
Length
INA
Width
INA
Height
INA
Weight, Combat
INA
Ground Pressure
INA
Automotive (Chassis)
Engine Name
INA
Engine Type
INA
Engine Power
INA
Cruising Range
INA
Speed, Maximum Road
INA
Speed, Average Cross
INA
Speed Maximum Swim
INA
Fording Depth
INA
Communications
Primary
INA
Missile System
Transporter, Erector, Launcher
Name
INA
Type
Transporter erector launcher
Fire on the Move
No
Missile
Name
Naze'at 6-H rocket
Type
SS Ballistic Missile / Long-Range Artillery Rocket
Length
6,290 mm
Diameter
356 mm
Initial Weight
960 kg
Propellant Weight
420 kg
Propellant Type
Solid Hydroxyl-terminated polybutadiene
Warhead Weight
130 kg
Maximum Range
100 km
Minimum Range
80 km
CEP
500-1000 m
Average Action Time
9 seconds
Specific Impulse
240 seconds
Service Life
7 Years
Speed
Mach 4-5
Fire Control
Note
No Guidance System however, TELs use GPS to set the launch site
Protection
Note (1)
The TEL has no active or passive protection systems other than NBC
Note (2)
The rocket has no counter measures
Details
Country of Origin
Iran
Category
Ground-Launched Ballistic Missiles (GLBM) (50 km - 300 km)
Air > Ground-Launched Ballistic Missiles (GLBM) (50 km - 300 km)
Filter Label
N
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
6.29 m
Width
0.36 m
Height
—
Weight
960 kg
Operators (2)
Iran
Non-State Actors
Something went wrong. Please reload the page.
Reload