Shock absorbers

Aeronautics and astronautics – Missile stabilization or trajectory control – Remote control

Patent

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Details

F41G 732

Patent

active

057204489

ABSTRACT:
This invention relates to a shock absorber for use with a command link controlled missile system. The shock absorber being designed to absorb the shocks produced by launch and missile movements and being particularly applicable to fibre optic command link systems.

REFERENCES:
patent: 3156185 (1964-11-01), Hermann et al.
patent: 4770370 (1988-09-01), Pinson
patent: 4796833 (1989-01-01), Pinson
patent: 4860968 (1989-08-01), Pinson

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