Invention Grant
- Patent Title: Missile launch system and apparatus therefor
- Patent Title (中): 导弹发射系统及其装置
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Application No.: US11647737Application Date: 2006-12-29
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Publication No.: US08256339B1Publication Date: 2012-09-04
- Inventor: Ari Hamalian , Alexander Cosmas
- Applicant: Ari Hamalian , Alexander Cosmas
- Applicant Address: US MD Bethesda
- Assignee: Lockheed Martin Corporation
- Current Assignee: Lockheed Martin Corporation
- Current Assignee Address: US MD Bethesda
- Agency: Howard IP Law Group, PC
- Main IPC: F41F3/04
- IPC: F41F3/04

Abstract:
A missile is guided and/or supported within a canister by a collapsible support structure. In one embodiment the collapsible support structure is part of a railcar running on a rail within the canister. Each railcar includes a missile-engaging guidance and/or support structure, a rail engaging element, and a hinged pantograph-like collapsible support extending between the missile-engaging structure and the rail engaging element. A hinge of the pantograph is locked in a storage state and during part of motion during the missile launch. The hinge is unlocked, and travel of the rail engaging element is stopped. The missile-engaging support structure momentarily continues its motion, and the pantograph collapses. Capture elements engage parts of the railcar or the canister during collapse to prevent rebound of the missile-engaging support structure toward the missile.
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