Stress reduction device for optical waveguide for aerial remote control of missile - guides waveguide to missile for signal transmission until detonation using tension-relieving winding in ejection tube

摘要

The optical waveguide (12) is connected to the guided missile (FK) and signal transmission is ensured up to the combat charge detonation. An unloading winding is located in the discharge base (11) thrust-out tube (11a). A stretch winding (13) is wound around the outer surface (17a) of the missile thrust-out container (17). Via guide loops the stretch winding goes as far as the thrust-out mouth of the missile thrust-out container (17) and is guided into the missile (FK). The discharge winding (16) for the missile (FK) is located in one of the segments (18), which are blown up by the gas pressure arising as the result of ignition of the missile drive mechanism, simultaneously freeing the winding (16). USE - E.g. for submarine missile launcher.