Electrically conducting reinforced optical fiber

Claim 2

Cable apparatus for providing combined large bandwidth optical signal communication and electric power transmission between two spaced locations, the cable comprising: an integral centrally located elongated fiber core of a first glass material for transmitting optical signals, said first glass material having a first refractive index; an integral layer of a glass-like material intimately surrounding said fiber core, said glass-like material having a second refractive index less than said first refractive index; a coating layer of a plastic material intimately surrounding said glass-like material layer; conductor means for transmitting electrical power embedded in said coating layer; and reinforcing means embedded in said coating layer.

Claim 3

The apparatus as in claim 1 wherein said conductor means includes a plurality of individual conductive members extending generally parallel to, and circumferentially spaced around, said core.

Claim 4

The apparatus as in claim 2 wherein at least one of said individual conductive members is separately insulated.

Claim 5

The apparatus as in claim 1 wherein said conductor means includes at least one circumferentially continuous tubular conductive sheath embedded in said coating layer.

Claim 6

The apparatus as in claim 4 further including another circumferentially continuous tubular conductive sheath positioned between said glass-like material layer and said coating layer and radially spaced inwardly from said one sheath.

Claim 7

The apparatus as in claim 1 wherein said reinforcing means includes reinforcing fibers embedded in said coating layer.

Claim 8

Apparatus for interconnecting a missile launch device with a remote missile launch control station, the apparatus comprising: a cable for transmitting electrical power and optical control signals from the control station to the launch device, said cable including (i) an integral centrally located elongated fiber core of a first glass material for transmitting optical signals, said first glass material having a first refractive index, (ii) an integral layer of glass-like material intimately surrounding said core, said glass-like material having a second refractive index less than said first refractive index, (iii) a coating layer of a glass-like material intimately surrounding said glass-like material layer, (iv) conductor means embedded in said coating layer for transmitting electrical power, and (v) reinforcing means embedded in said coating layer, said cable also including respective end portions proximate the controller station and the launch device; and said terminating means including respective electrical connectors and optical fiber connectors connected to the control station and the launch device.

Claim 9

Apparatus for interconnecting a missile launch device with a remote missile launch control station, the apparatus comprising: a cable for transmitting electrical power and optical control signals from the control station to the launch device, said cable including (i) an integral centrally located elongated fiber core of a first glass material for transmitting optical signals, said first glass material having a first refractive index, (ii) an integral layer of glass-like material intimately surrounding said core, said glass-like material having a second refractive index less than said first refractive index, (iii) a coating layer of a glass-like material intimately surrounding said glass-like material layer, (iv) conductor means embedded in said coating layer for transmitting electrical power, and (v) reinforcing means embedded in said coating layer, said cable also including respective end portions proximate the controller station and the launch device; and said terminating means including respective electrical connectors and optical fiber connectors connected to the control station and the launch device.

Claim 10

The interconnecting apparatus as in claim 7 wherein at least the electrical connector associated with the launch device is a breakaway-type electrical connector.

Claim 11

The interconnecting apparatus as in claim 7 wherein at least the portion of the conductor means received at the launch device is configured as a pigtail.

Claim 12

The interconnecting apparatus as in claim 7 wherein at least the portion of the conductor means received at the launch device is separately electrically insulated.

Claim 13

The interconnecting apparatus as in claim 7 wherein said terminating means includes a step-dwown transformer and rectifier operatively connected to the received portion of the conductor means proximate the launch device.