FIELD: rocket launchers.
SUBSTANCE: invention relates to rocket launchers, particularly, to means for disconnection of electrical connection between missile and transport-launch container (TLC). Electric connector retraction mechanism comprises a hinged four-link mechanism in the form of a parallelogram with a lever-spring mechanism enclosed in it, a plug pressed by devices of a gap-free electric connection, and a socket.
EFFECT: higher reliability and convenience of electric connection of missile and TLC.
1 cl, 4 dwg
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|---|---|---|---|
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| LAUNCHING SYSTEM | 2009 |
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| ROCKET IN LAUNCHING PACK | 2003 |
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| ROCKET-TORPEDO LAUNCHER | 1998 |
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| LAUNCHER | 2006 |
|
RU2309362C1 |
