Hsiung Feng IIE
XXACTIVE弹道导弹
技术参数
| — | 10 to 15 m}} | 低 | |
| — | |guidance=GPS, TERCOM, and inertial guidance with automatic target recognition for terminal guidance | 低 | |
| — | |filling= | 低 | |
| — | Various reported ranges from 600 km to >2,000km >1200 km for Hsiung Sheng | 低 | |
| — | turbofan with solid rocket booster | 低 | |
| — | |speed= (Mach 0.75 - 0.85) | 低 | |
| — | |diameter=20 in | 低 | |
| — | 236 in | 低 | |
| — | 3500 lb | 低 | |
| — | |production_date= ~300 (2012), in production | 低 | |
| — | ~3m USD (2003) | 低 | |
| — | National Chung-Shan Institute of Science and Technology | 低 | |
| — | Republic of China (Taiwan) Armed Forces | 低 | |
| — | 2011 – present | 低 | |
| — | Land-attack cruise missile | 低 | |
| — | Taiwan | 低 | |
| — | Hsiung Feng IIE | 低 | |
| — | yes | 低 | |
| name | {'is_missile': 'yes', 'name': 'Hsiung Feng IIE', 'image': '|caption=', 'origin': 'Taiwan', 'type': 'Land-attack cruise missile', 'service': '2011 – present', 'used_by': 'Republic of China (Taiwan) Armed Forces', 'manufacturer': 'National Chung-Shan Institute of Science and Technology', 'unit_cost': '~3m USD (2003)', 'propellant': '|production_date= ~300 (2012), in production', 'weight': '3500 lb', 'length': '236 in', 'height': '|diameter=20 in', 'wingspan': '|speed= (Mach 0.75 - 0.85)', 'engine': 'turbofan with solid rocket booster', 'vehicle_range': 'Various reported ranges from 600 km to >2,000km >1200 km for Hsiung Sheng', 'ceiling': '|filling=', 'detonation': '|guidance=GPS, TERCOM, and inertial guidance with automatic target recognition for terminal guidance', 'accuracy': '10 to 15 m}}'} | 低 |