Gabriel III
| Specifications | ||
|---|---|---|
| Contractor | Israeli Aircraft Industries | |
| 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 | |
| Propulsion | single stage solid propellant rocket motor or liquid fuel turbojet | |
| Maximum Speed | 840 km/h | |
| Maximum effective range |
Ceiling: 9100 m Maximum range (rocket motor): 40 km Maximum range (turbojet motor): 60 km | |
| Guidance mode | I-band active radar | |
| Single-shot hit probability | ||
