12-05-2023 дата публикации
Номер: CN116105554A
Принадлежит:
The terminal guided rocket projectile comprises a head cover, a seeker, a control cabin, a warhead and a rocket engine which are sequentially arranged from the head to the tail, and a falling-off socket is arranged on the control cabin; the test socket is in signal connection with the control cabin through a CAN bus; and the test socket and the drop-off socket are symmetrically arranged by taking the central axis of the control cabin as a symmetry axis. As the test socket is additionally provided with the transmission node, original data can be directly obtained, and the transmission speed is high, so that the launching preparation time is short, the test can be quickly completed before launching, and the launching efficiency can be improved. Besides, the test socket and the drop-off socket are symmetrically arranged by taking the central axis of the control cabin as a symmetry axis, so that asymmetric aerodynamic torque can be eliminated, and the rocket projectile can fly more stably; ...
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