Annular shock absorbing system for a missile launcher

Ordnance – Rocket launching – Having tubular guide means

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89 1809, F41F 304

Patent

active

044062117

ABSTRACT:
A 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.

REFERENCES:
patent: 3072022 (1963-01-01), Wood et al.
patent: 3124040 (1964-03-01), Fiedler
patent: 3135162 (1964-06-01), Kamalian
patent: 3221602 (1965-12-01), Price et al.
patent: 3289533 (1966-12-01), Brown
patent: 3367235 (1968-02-01), Andrews
patent: 3392629 (1968-07-01), Soderberg
patent: 3499364 (1970-03-01), D'Ooge
patent: 3857321 (1974-12-01), Cohen

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