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Popeye-3

Country:  Israel
Alternate Name:  Popeye Turbo
Class:  ALCM
Target:  Land
Propulsion:  Turbojet
Range:  300.00 km
Guidance:  INS, GPS
Status:  Operational
In Service:  2002-Present

Details

The Popeye-3 is a short-range, television or imaging infrared-guided, air-to-surface cruise missile proposed by Israel to Great Britain in 1994. It was planned to be fitted with a turbofan engine, which would give the Popeye-3 a maximum range in excess of 200 km. Britain did not select the Popeye-3, although reports from 1998 indicate that Israel was continuing with design studies for a turbojet powered Popeye-3.

If developed, the Popeye-3 would be part of the same family of Israeli missiles as the air-launched AGM-142 Popeye-1 “Have Nap” and Popeye-2 “Have Lite.”(1)

 

 

 

 

Footnotes

 

  1. Duncan Lennox, ed., Jane’s Strategic Weapons Systems 45 (Surrey: Jane’s Information Group, July 2006), pp. 75-77; GlobalSecurity.org, “AGM-142 Raptor / Popeye I Have Nap / Popeye II Have Lite,” available at http://www.globalsecurity.org/military/systems/munitions/agm-142.htm, accessed on July 1, 2006.

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