Jericho I  
Initial Operational Capability (IOC): 1971
Total Production: 100
Origin: Israel
Corporations: Israel Aerospace Industries Ltd. (IAI)
Parent System: Jericho
Initial Operational Capability (IOC): 1971
Total Production: 100
Family Members: Jericho II and Jericho III
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Description: The Jericho is a Short Range Ballistic Missile developed based in French technology in the 1960s and deployed by Israel during the 1970s. It has a range of 500 kilometers carrying a 500 kg nuclear or chemical payload. Its primary role is to provide deterrence against Arab nations that could threaten Israel. It was retired from active service in the 1990s and replaced by the more capable Jericho II ballistic missile.

Jericho I Specifications

Number of Stages: 1
Number of Warheads: 1
Diameter: 0.80 meter (31.5 inch)
Length: 13.4 meter (528 inch)
CEP: 1,000 meter
Max Range: 500 kilometer (270 nautical mile)
Warhead: 500 kilogram (1,102 pound)
Weight: 6,500 kilogram (14,330 pound)
CEP: Circular Error Probable
Meters (m)   Kilometers (km)   Nautic Miles (nm)   Inch (in)   Yard (yd)   Foot (ft)   Millimeter (mm)
Pound (lb)   Kilogram (kg)   kN (KiloNewton)   Ton (t)
Meters per Second (mps)   Kilometers per Hour (kph)   Knot (kt)   Miles per Hour (mph)
Liter (l)   Galon (gl)
Year (yr)   Minutes (min)   Second (sec)
Shaft-Horse-Power (shp)

Operators & Related Equipment


Grand Total 1001
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