AGM-86
XXACTIVE弹道导弹
技术参数
| — | | launch_platform = Boeing B-52H Stratofortress }} | 低 | |
| — | 908kg (AGM-86C Block 0) 1362kg (AGM-86C Block 1) 1,200 lb class advanced unitary penetrating warhead (AGM-86D) | 低 | |
| — | AGM-86B: Litton inertial navigation system element with TERCOM updates AGM 86C: Litton INS element integrated with multi-channel onboard GPS AGM-86C Block 0, 2,000 lb. (900 kg) class, Block I, 3,000 lb. (1,400 kg) class-->| filling = W80 thermonuclear weapon (AGM-86B), 5 or 150 kilotons Conventional warhead (AGM-86C) AUP warhead (AGM-86D) | 低 | |
| — | | altitude = | 低 | |
| — | AGM-86B: 1,500+ mi (2,400+ km)AGM-86C: classified (nominal 680 miles, 1,100 km) | 低 | |
| — | AGM-86B: 550 mph (890 km/h, Mach 0.73)AGM 86C: classified (nominal high subsonic) | 低 | |
| — | 12 ft | 低 | |
| — | | diameter = 24.5 in | 低 | |
| — | 20 ft. 9 in. (6.3 m) | 低 | |
| — | 1,458 kg (AGM-86B) 1,750 kg (AGM-86C Block 0 and AGM-86D) 1,950 kg (AGM-86C Block 1) | 低 | |
| — | 600 lbf (2.7 kN) thrust | 低 | |
| — | Williams InternationalF107-WR-101 turbofan engine | 低 | |
| — | 1,715 (AGM-86B) 239 (AGM-86C) 50 (AGM-86D) | 低 | |
| — | 1980 | 低 | |
| — | | design_date = 1974 | 低 | |
| — | $1 million (AGM-86B)additional $160,000 conversion cost for AGM-86C;additional $896,000 conversion cost for AGM-86D | 低 | |
| — | Boeing Integrated Defense Systems | 低 | |
| — | United States Air Force | 低 | |
| — | AGM-86B: 1982–presentAGM-86C/D: retired | 低 | |
| — | Air-to-ground strategic cruise missile | 低 | |
| — | United States | 低 | |
| — | AGM-86 | 低 | |
| — | yes | 低 | |
| name | {'is_missile': 'yes', 'name': 'AGM-86', 'image': 'AGM-86 ALCM.JPEG', 'caption': 'An AGM-86C in flight', 'origin': 'United States', 'type': 'Air-to-ground strategic cruise missile', 'service': 'AGM-86B: 1982–presentAGM-86C/D: retired', 'used_by': 'United States Air Force', 'manufacturer': 'Boeing Integrated Defense Systems', 'unit_cost': '$1 million (AGM-86B)additional $160,000 conversion cost for AGM-86C;additional $896,000 conversion cost for AGM-86D', 'propellant': '| design_date = 1974', 'production_date': '1980', 'variants': 'AGM-86B (1982), AGM-86C (1991), AGM-86D (2001)', 'number': '1,715 (AGM-86B) 239 (AGM-86C) 50 (AGM-86D)', 'engine': 'Williams InternationalF107-WR-101 turbofan engine', 'engine_power': '600 lbf (2.7 kN) thrust', 'weight': '1,458 kg (AGM-86B) 1,750 kg (AGM-86C Block 0 and AGM-86D) 1,950 kg (AGM-86C Block 1)', 'length': '20 ft. 9 in. (6.3 m)', 'height': '| diameter = 24.5 in', 'wingspan': '12 ft', 'speed': 'AGM-86B: 550 mph (890 km/h, Mach 0.73)AGM 86C: classified (nominal high subsonic)', 'vehicle_range': 'AGM-86B: 1,500+ mi (2,400+ km)AGM-86C: classified (nominal 680 miles, 1,100 km)', 'ceiling': '| altitude =', 'guidance': 'AGM-86B: Litton inertial navigation system element with TERCOM updates AGM 86C: Litton INS element integrated with multi-channel onboard GPS AGM-86C Block 0, 2,000 lb. (900 kg) class, Block I, 3,000 lb. (1,400 kg) class-->| filling = W80 thermonuclear weapon (AGM-86B), 5 or 150 kilotons Conventional warhead (AGM-86C) AUP warhead (AGM-86D)', 'filling_weight': '908kg (AGM-86C Block 0) 1362kg (AGM-86C Block 1) 1,200 lb class advanced unitary penetrating warhead (AGM-86D)', 'detonation': '| launch_platform = Boeing B-52H Stratofortress }}'} | 低 |