Arrow
| Specifications | ||
|---|---|---|
| Designer | Israel Aerospace Industries | |
| Designed | 1994–present | |
| Manufacturer | Israel Aerospace Industries, Boeing | |
| Model | Arrow 2 | Arrow 3 |
| Middle Tier | Upper Tier | |
![]() | ||
| Unit cost | US$3 million (2003) | ... |
| Produced | 2000–present | 2016-present |
| Components |
|
|
| Weight |
|
[rough estimate] |
| Length |
|
[rough estimate] |
| Diameter By stage |
|
|
| 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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