Rocket fin hold down spring

Aeronautics and astronautics – Missile stabilization or trajectory control – Externally mounted stabilizing appendage

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Details

F42B 1332

Patent

active

043846912

ABSTRACT:
A missile disposed for launching from a telescoping launcher having inner d outer sections. The missile is provided with fins folded along the body. A resilient spring clip member is carried on each said fin and engages the inner surfaces of the launcher sections as the missile traverses the launcher to retain the fins in folded position in the launcher.

REFERENCES:
patent: 3690595 (1972-09-01), Rusbach
patent: 3754726 (1973-08-01), Rusbach
patent: 3819132 (1974-06-01), Rusbach
patent: 3918664 (1975-11-01), Grosswendt

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