Kh-55/65/555AS-15 Kent
XXACTIVE弹道导弹
技术参数
| — | Tu-95MS, Tu-160, Su-34 }} | 低 | |
| — | inertial guidance with Doppler radar/terrain map updates; Kh-SD had a TC/IIR terminal guidance system, and an alternative active radar homing seeker was proposed | 低 | |
| — | 200kt Nuclear (Kh-55/Kh-55SM) | 低 | |
| — | Thermonuclear weapon or Conventional warhead | 低 | |
| — | under 110 m/300 ft | 低 | |
| — | 2500 km (Kh-55)3000 km (Kh-55SM)600 km (Kh-65SE)300 km, later 600 km (Kh-SD) | 低 | |
| — | Mach 0.75 (KH-SD)Mach 0.6-0.78 (Kh-101) | 低 | |
| — | 310 cm (Kh-55/Kh-55SM) | 低 | |
| — | 51.4 cm (Kh-55/Kh-55SM) | 低 | |
| — | 604 cm (Kh-65SE)745 cm (Kh-101) | 低 | |
| — | 1650 kg (Kh-65SE) | 低 | |
| — | 360-400 kgf (Kh-55/Kh-55SM) | 低 | |
| — | R95TP-300 Turbofan/turbofan (Kh-55/Kh-55SM) | 低 | |
| — | 1983–present | 低 | |
| — | 1981 | 低 | |
| — | jet fuel | 低 | |
| — | Raduga OKB, KhAZ (Kharkiv), Novator (MZiK) & NPP Temp (Eka) NPO Strela (Oren), else | 低 | |
| — | 1971–1981 | 低 | |
| — | Syrian Civil WarRusso-Ukrainian war | 低 | |
| — | Soviet Union, Russia, China, Iran | 低 | |
| — | Air-launched cruise missile | 低 | |
| — | Soviet Union | 低 | |
| — | Kh-55/65/555AS-15 Kent | 低 | |
| — | yes | 低 | |
| name | {'is_missile': 'yes', 'name': 'Kh-55/65/555AS-15 Kent', 'image': 'H-55 AS-15 Kent 2008 G1.jpg', 'image_size': '300px', 'caption': 'Kh-55 in the Ukrainian Air Force Museum', 'origin': 'Soviet Union', 'type': 'Air-launched cruise missile', 'used_by': 'Soviet Union, Russia, China, Iran', 'wars': 'Syrian Civil WarRusso-Ukrainian war', 'design_date': '1971–1981', 'manufacturer': 'Raduga OKB, KhAZ (Kharkiv), Novator (MZiK) & NPP Temp (Eka) NPO Strela (Oren), else', 'propellant': 'jet fuel', 'production_date': '1981', 'service': '1983–present', 'engine': 'R95TP-300 Turbofan/turbofan (Kh-55/Kh-55SM)', 'engine_power': '360-400 kgf (Kh-55/Kh-55SM)', 'weight': '1650 kg (Kh-65SE)', 'length': '604 cm (Kh-65SE)745 cm (Kh-101)', 'diameter': '51.4 cm (Kh-55/Kh-55SM)', 'wingspan': '310 cm (Kh-55/Kh-55SM)', 'speed': 'Mach 0.75 (KH-SD)Mach 0.6-0.78 (Kh-101)', 'vehicle_range': '2500 km (Kh-55)3000 km (Kh-55SM)600 km (Kh-65SE)300 km, later 600 km (Kh-SD)', 'altitude': 'under 110 m/300 ft', 'filling': 'Thermonuclear weapon or Conventional warhead', 'yield': '200kt Nuclear (Kh-55/Kh-55SM)', 'guidance': 'inertial guidance with Doppler radar/terrain map updates; Kh-SD had a TC/IIR terminal guidance system, and an alternative active radar homing seeker was proposed', 'launch_platform': 'Tu-95MS, Tu-160, Su-34 }}'} | 低 |