Aeronautics and astronautics – Missile stabilization or trajectory control – Remote control
Patent
1995-04-05
1996-10-15
Carone, Michael J.
Aeronautics and astronautics
Missile stabilization or trajectory control
Remote control
114 211, 102504, F41G 732
Patent
active
055646492
ABSTRACT:
The invention provides an apparatus for the remote control of missiles or torpedoes launched from a launching container, by means of a cable of which a portion is wound onto a supply reel connected with the launching and of which the other portion is wound onto a supply reel in the missile or the torpedo. The supply reel in the launching container is arranged on the forward end of the container, and the supply reel in the missile or torpedo is arranged on the rearward end of the missile or torpedo. The cable section between the two supply reels, before the launching of the missile or torpedo, is fastened along the major portion of its length on the interior wall of the launching container, by means of a gluing arrangement which consists of a material whose combustion temperature is at least by 800.degree. C. lower than the melting temperature of the optical waveguide, or by means of a flexible clamping arrangement whose holding force can be adjusted.
REFERENCES:
patent: 3265023 (1966-08-01), Hollingsworth, Jr. et al.
patent: 4573647 (1986-03-01), Laten et al.
patent: 5022607 (1991-06-01), Schotter
patent: 5031997 (1991-07-01), Redford et al.
Seiffarth Ernst-August
von Hoessle Wolfgang
Carone Michael J.
Daimler-Benz Aerospace AG
Montgomery Christopher K.
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