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公开(公告)号：KR860000221B1
公开(公告)日：1986-03-15
申请号：KR820004172
申请日：1982-09-15
Applicant: GEN DYNAMICS CORP
Inventor： OLDHAM DELBERT J , CARISH JOHN A
Abstract: The launcher has a central support frame with attachment points that permit attachment to the aircraft or other launching platform. It has a central frame with a launch tube saddle-support assembly at each side of the frame, quick-detachable clamps and an alignment guide for quickly positioning and securing the launch tubes into position, auto connectors for automatically connecting the electronic control system and coolant gas to the launch tube assembly when the assembly is clamped into position. An aerodynamically shaped shell is used to enclose the support structure and the electronic control system.
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