| 摘要 |
<p>PURPOSE:To obtain a missile in which directionality of a nose power can be incorporated in any direction with a simple structure. CONSTITUTION:A directional nose having one initiator cylinder is provided at a position apart from a center in a missile. Further, the missile has a circuit 21 for so calculating a rolling angle and a rolling direction of a body that directional nose power from target direction information collected by a seeker 20 coincides with a target direction.</p> |
