Filament payout apparatus

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

Patent

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Details

89 134, 102504, F41G 732

Patent

active

050297724

ABSTRACT:
A drumlike canister onto which a filament is wound is rotatably mounted to an airborne vehicle, the axis of rotation being generally parallel to the vehicle longitudinal axis. At launch, as the filament unwinds and is payed out the canister is rotated to remove the twist from the filament produced on winding.

REFERENCES:
patent: 2469533 (1949-05-01), Wellcome
patent: 4770370 (1988-09-01), Pinson
patent: 4817529 (1989-04-01), Schippers

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