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Surface-to-surface missile
Taiwan
Early 1990s-present
Republic of China Armed Forces
National Chung-Shan Institute of Science and Technology
Air launched version without first stage rocket booster
685 kg (1,510 lb)
4,800 mm (190 in)
400 mm (16 in)
180 kg (400 lb)
160 km (99 mi) (Block 1) 250 km (160 mi) (Block 2)
1,041 km/h (647 mph)
Inertial guidance midflight, terminal with dual active radar homing and infrared homing seekers
Box launcher or aircraft
Reference text from Wikipedia contributors, used under CC BY-SA 4.0.
Hsiung Feng II equipment records. Variants, orders and quantities are shown as reported in each inventory source; coverage is incomplete.