Arrow
Specifications | ||
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Designer | Israel Aerospace Industries | |
Designed | 1994–present | |
Manufacturer | Israel Aerospace Industries, Boeing | |
Model | Arrow 2 | Arrow 3 |
Middle Tier | Upper Tier | |
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Unit cost | US$3 million (2003) | ... |
Produced | 2000–present | 2016-present |
Components |
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Weight |
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[rough estimate] |
Length |
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[rough estimate] |
Diameter By stage |
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Wingspan | 820 mm (32 in) | nil |
Motors | Two-stage | Two-stage |
Propellant | Solid propellant | Solid propellant |
Operational range | 90 km (56 mi) – 150 km (93 mi) | ... |
Flight ceiling | 50 km (31 mi) – 60 km (37 mi) | anti-satellite (Asat) capability. |
Speed | Mach 9, 2.5 km/s (1.6 mi/s) | ... |
Warhead | Directed high explosive fragmentation | “body-to-body” “hit-to-kill” |
Warhead weight | 150 kg (330 lb) | ... |
Detonation mechanism | Proximity fuze | none - hit to kill |
Guidance system | Dual mode passive infrared seeker + active radar seeker | ... |
Steering system | Thrust vectoring + four aerodynamic control moving fins | thrust-vectoring |
Accuracy | Within 4 m (13 ft) of the target | hit to kill |
Launch platform | Six canisters per trailer-mounted erector–launcher | fixed hardened site |
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