 | Shahine
| Surface-to-air missile. Year: 1980. IOC: 1980. Country: France. Model: R.460. IOC: 1980. Country: France. Total Mass: 90 kg (198 lb). Core Diameter: 0.15 m (0.49 ft). Total Length: 3.03 m (9.94 ft). Span: 0.53 m (1.73 ft). Standard warhead mass: 15 kg (33 lb). Maximum range: 10 km (6 mi). Boost Propulsion: Solid rocket. Guidance: Beam rider + Command Link. Maximum speed: 2,820 kph (1,750 mph). Minimum range: 0.50 km (0.31 mi). Ceiling: 3,000 m (9,800 ft). Floor: 50 m (164 ft). Surveillance Radar: E/F Band. Tracking Radar: PD/MTI. Total Number Built: 1000. Model: SA.10. IOC: 1980. Country: France. 6 launcher/vehicle. Program ended. Manufacturer: MATRA BAe Dynamics. Location: London, UK. Guidance contractor: Thomson-CSF. Total Mass: 106 kg (233 lb). Core Diameter: 0.15 m (0.50 ft). Total Length: 3.20 m (10.50 ft). Span: 0.55 m (1.80 ft). Maximum range: 15 km (9 mi). Boost Propulsion: Solid rocket. Guidance: Command Link. Maximum speed: 2,600 kph (1,600 mph). Minimum range: 0.50 km (0.31 mi). Floor: 50 m (164 ft). Surveillance Radar: S band. Tracking Radar: Ku band.
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