| 摘要 |
<p>The missile (1) has a missile casing (3) forming an outer contour of the missile and extending along a longitudinal direction. The missile casing is formed for accommodated a set of units that include a sensor unit (5), a propulsion unit (7) and a payload unit (8), where two of the units are attached in parallel in the longitudinal direction. The payload unit is arranged at an overall center of gravity (S) of the missile. The missile casing is formed of a plastic reinforced with carbon fiber, and one of the units is formed as an interchangeable module. The set of units include the sensor unit e.g. electro-optical, infrared, radar or ladar seeker head, the propulsion unit e.g. turbine motor, solid-fuel motor or gel-fuel motor, and the payload unit e.g. shape-charged unit or high power microwave unit (HPMW) unit. The turbine motor is a solid-fuel motor having a motor structure formed from a fiber composite material e.g. plastic reinforced with carbon fibers material.</p> |
