Hybrid unitized shock and vibration mitigation system

Details Hybrid unitized shock and vibration mitigation system Hybrid unitized shock and vibration mitigation system

1985-06-03

1986-12-09

Brown, David H.

Ordnance

Rocket launching

Having tubular guide means

89 1810, F41F 304

Patent

active

046273271

ABSTRACT:
A system for reducing the shock and vibration transmitted to a missile dug transportation, stowage or launch. Rings of segmented shock-absorbing pads are disposed along the launch tube in the annular space between the missile and the tube. These pad segments are unitized by a circumferential tensile fiber hoop connecting the pad segments, and portions of this unitizing hoop are used to form control loops between these pad segments. The loop characteristics may be selectively varied to control the effective modulus and circumferential length of each unitizing hoop thus varying the force/deflection characteristics of the pad ring.

REFERENCES:
patent: 3072022 (1963-01-01), Wood et al.
patent: 3166978 (1965-01-01), Price et al.
patent: 3289533 (1966-12-01), Brown
patent: 3392629 (1968-07-01), Soderberg
patent: 3823903 (1974-07-01), Kendall et al.
patent: 3857321 (1974-12-01), Cohen
patent: 4399999 (1983-08-01), Wold
patent: 4406211 (1983-09-01), Andersen
patent: 4433848 (1984-02-01), Williams
patent: 4485719 (1984-12-01), Mendelsohn et al.

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