Unitized shock isolation and missile support system

Details Unitized shock isolation and missile support system Unitized shock isolation and missile support system

1985-01-18

1993-06-15

Brown, David H.

Ordnance

Rocket launching

Having tubular guide means

89 1809, F41F 304

Patent

active

052201252

ABSTRACT:
A unitized shock isolation and support system disposed in an annular space between two cylindrical surfaces utilizing a first compressible portion axially oriented chevron-shaped prebuckled struts to support a rigid or semirigid hoop larger in diameter than the inner cylinder and second compressible portion or a foam liner disposed on the inner diameter of the hoop, the foam liner being thicker than the annular space between the inner cylinder and the hoop to form a space efficient system mitigating shock and for laterally supporting the inner cylindrical surface within the outer cylindrical surface.

REFERENCES:
patent: 3072022 (1963-01-01), Wood et al.
patent: 3124040 (1964-03-01), Fiedler
patent: 3166978 (1965-01-01), Price et al.
patent: 3289533 (1966-12-01), Brown
patent: 3367235 (1968-02-01), Andrews
patent: 3857321 (1974-12-01), Cohen
patent: 3899260 (1975-08-01), Kerschner
patent: 4118019 (1978-10-01), Weir
patent: 4399999 (1983-08-01), Wold
patent: 4406211 (1983-09-01), Anderson
patent: 4433848 (1984-02-01), Williams

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