Specifications
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| Contractor | Israeli Aircraft Industries
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| Entered Service | 1982
|
|
Modifications |
Solid propellant rocket motor
Liquid fuel turbojet motor
|
| Total length | 3.9 m
|
| Diameter | 0.34 m
|
| Wingspan | 1.1 m
|
| Weight | 600 kg
|
| Warhead | contact-, graze- and deceleration-fuzed high-explosive, 150 kg
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| Propulsion | single stage solid propellant rocket motor or liquid fuel turbojet
|
| Maximum Speed | 840 km/h
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| Maximum effective range |
Ceiling: 9100 m
Maximum range (rocket motor): 40 km
Maximum range (turbojet motor): 60 km
|
| Guidance mode | I-band active radar
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| Single-shot hit probability |
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