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Military


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 




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