Aeronautics and astronautics – Missile stabilization or trajectory control – Remote control
Patent
1991-02-01
1992-09-01
Jordan, Charles T.
Aeronautics and astronautics
Missile stabilization or trajectory control
Remote control
F41G 732
Patent
active
051433192
ABSTRACT:
A length of filament (32), wire or optical fiber, is wound into a pack (30) on a cylindrical drum (44) located within an open-ended housing (38). The housing is mounted within a missile (26) with the housing open end (38) facing aft. An undersized front wall (48) fits over the enclosure open end leaving a circular gap or space (50) through which the filament is dispensed. An outer end portion of the filament is reinforced (42) both mechanically and thermally to allow dispensing through outer regions of the missile rocket plume. The walls defining the circular gap (50) brake the filament dispensing to a predetermined maximum speed.
REFERENCES:
patent: 3233548 (1966-02-01), Chilowsky
patent: 4903607 (1990-02-01), Clark
patent: 4974793 (1990-12-01), Pinson
Brown C. D.
Denson-Low W. K.
Heald R. M.
Hughes Aircraft Company
Jordan Charles T.
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