Patent References 3072022 3124040 3135162 3221602 3289533 3367235 3392629 3499364 3857321 InventorAssigneeApplicationNo. 06/287611 filed on 07/28/1981US Classes:89/1.816, Having tubular guide means89/1.809Underwater launchingExaminersPrimary: Brown, David H.Attorney, Agent or FirmInternational ClassesF41F 3/00 (20060101)F41F 3/073 (20060101) AbstractA shock absorbing pad system for a missile launch tube, wherein the shock absorbing pad system comprises a continuously acting inner sheet, an outer segmented sheet and a plurality of chevron shaped struts disposed between the sheets. The continuously acting inner sheet provides compressive, shear, and tensile forces or a combination thereof to resist lateral shock loads and to restore the missile to its central location within the launch tube. | |