Abstract: An optical fiber dispensing system (30) includes a canister (42) within which an optical fiber (12) is wound, and a helix dampener (40) that reduces the helical diameter of the optical fiber (12) as it is paid out from the canister (42) along a payout axis (20). The canister (42) is either a cylinder or a slightly tapered cone. The helix dampener (40) is a structure overlying the payout end of the canister (42) and extending beyond the canister (42) along the payout axis (20). The interior surface of the helix dampener (40) defines a locus (36) of points whose distance from the payout axis (20) decreases with increasing distance from the canister (42), to an opening (38) through which the optical fiber (12) is dispensed.

Abstract: An optical fiber (18) payout system for a missile (10) which is to be hot-launched from a tube (12) reinforces that part of the fiber to be exposed to propulsion gases by juxtaposing with one or more wires (24) and encasing within a thermally protective sheath (22) forming a so-called leader (20). The leader (20) extends outwardly of the missile aft end (16) and is releasably secured within a rail assembly (32) by a flexible strip (46) having a line of perforations (48) extending along its longitudinal axis. The outer end portion of the leader (20) is secured to an anchor block (52). On launch, the leader (20) tears loose from the flexible strip (46), the restraining action of which prevents optical fiber predispensing.

Abstract: A method and apparatus for pulling fiber from a bobbin using a payout wheel dispensing the fiber into the air in a helical pattern. The invention includes a deflector mounted in the path of the fiber which is rotated as the fiber is payed out. The deflector includes a hollow shaft through which fiber, from the wheel, passes. The hollow shaft includes a tunnel along the length thereof. The tunnel has a first portion, along the longitudinal axis of the shaft, and a second portion at an angle with respect to the first portion.

Abstract: An optical fiber bending stress proof tester 40 which provides multiple mandrels or roller elements 22 and 24 for applying compression and tension stresses to multiple planes on the periphery of an optical fiber 10. In one embodiment, first and second roller elements 22 and 24 are incorporated in a roller block 50 which is stable in either of two angular orientations with respect to the longitudinal axis of the fiber 10. The fiber 10 is bent in an S curve around the two rollers 22 and 24. The rollers 22 and 24 control the bend radius and therefore the stress induced in the outer fibers of the filament. In a specific extension of this embodiment, multiple sets of first and second roller elements are provided in additional roller blocks. Each block is stable in a first loading position and a second test position. In the test position, discrete planes around the entire periphery of the fiber are exposed to bending stress in a single pass through the tester.