Aeronautics and astronautics – Missile stabilization or trajectory control – Remote control
Patent
1990-12-04
1991-08-20
Jordan, Charles T.
Aeronautics and astronautics
Missile stabilization or trajectory control
Remote control
F41G 732
Patent
active
050407449
ABSTRACT:
A filament (20) for use as a data link is wound on the tapered aft fairing (22) of a missile (10) in a manner so as to form a tapered wound pack (24) conforming generally to the aft fairing. An outer length of the filament is enclosed within a protective covering forming a leader (26). When the missile is launched from a moving mother vehicle (36), a further length of the filament is wound onto a dispenser aboard the mother vehicle (36) and a drogue (30) connected to the leader (26) is released with the leader and filament during dispensing.
REFERENCES:
patent: 601604 (1898-03-01), Walsh
patent: 3266423 (1966-08-01), Simpson
patent: 3319781 (1967-05-01), Simpson et al.
patent: 4770370 (1988-09-01), Pinson
patent: 4860968 (1989-08-01), Pinson
patent: 4903607 (1990-02-01), Clark
Brown C. D.
Denson-Low W. K.
Heald R. M.
Highes Aircraft Company
Jordan Charles T.
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