| 摘要 |
FIELD: weapons and ammunition.SUBSTANCE: controlled missile with guidance laser beam is arranged in transport-launching container and comprises photodetector mounted near the nozzles of booster engine, closed disk attached to housing of photodetector destructible annular cage, and end seal arranged between disc and photodetector. Additionally between disc and optical element photodetector there is plate spring interacting with optical element on one side of photodetector, and other side with disc, closing photodetector. Spring can be made in form of rectangular bent along arc of circumference of plate. Between end seal and housing of photodetector there is circular gasket from resilient material.EFFECT: technical result is increased reliability due to timely opening of optical element photodetector after missile exit from transporter-launcher container for provision of its controlled flight.3 cl, 5 dwg |
