Trident (missile)
Jump to navigation
Jump to search
 | This article is incomplete because it is pending further input from participants, or it is a work-in-progress by one author. Please comment on this article's talk page to share your input, comments and questions. Note: To contribute to this article, you may need to seek help from the author(s) of this page. |
| Trident | |
|---|---|
 An AS-180 aircraft-launched Trident missile. | |
| Type | Anti-ship missile |
| Place of origin |  Hulie |
| Service history | |
| In service | 1974 |
| Used by | See Operators |
| Specifications | |
| Weight | 670 kilograms (1,480 lb) |
| Length | 4.7 metres (15 ft 5 in) |
| Diameter | 34.8 centimetres (1 ft 1.7 in) |
| Warhead | 165 kilograms (364 lb) |
| Engine | Turbojet Solid-propellant booster (SS-180/US-180 only) |
| Wingspan | 1.1 metres (3 ft 7 in) |
Operational range | 180 kilometres (97 nmi; 110 mi) |
| Flight altitude | Sea-skimming |
| Speed | Mach 0.92 1,134 kilometres per hour (705 mph; 315 m/s) |
Guidance system | Inertial guidance and terminal active radar homing |
Launch platform | Multi-platform:
|