Conmoly | CM-DATA-FIBER | Fiber Optic Cables
Shenzhen Xinju New Materials Technology Co., Ltd.
https://conmoly.com

Selection reference; third-party published figures are not Conmoly guaranteed specifications or certifications. Final specifications require configuration review. Images illustrate product form.
Reference configuration: Lightweight fiber-optic cable for aerospace and defense high-bandwidth interconnects, spanning singlemode and OM1–OM5 multimode directions through 100 Gb/s with PFA, FEP or PEEK jackets and buffered strength systems controlling optical loss, microbend and wide-temperature protection.

Optical loss, temperature and jacket material vary by diameter, fiber class and part number; the final specification must identify the exact part number.
Maximum data rate: 100 Gb/s | 1.8 / 1.2 / 0.9 mm simplex constructions
Maximum optical loss: ≤ 5.0 dB/km @ 850 nm | 1.8 mm multimode configuration limit
Maximum optical loss: ≤ 3.0 dB/km @ 1300 nm | 1.8 mm multimode configuration
Maximum optical loss: ≤ 1.5 dB/km @ 1300 nm | 1.2 mm configuration
Optical loss: 3.0 / 1.0 dB/km | 0.9 mm; 850 / 1310 nm
Operating temperature: −65 to +135 °C | 1.8 mm and 0.9 mm versions
Jacket / fiber classes: PFA · FEP · PEEK / SM · OM1–OM5 | Configuration dependent
Source: https://www.gore.com/products/fiber-optic-cables-aerospace-defense-air-land

1.8 mm rugged simplex: A protected multimode high-bandwidth channel with fuller buffer, strength and jacket layers.
1.2 mm lightweight simplex: Balances mechanical protection with small-diameter routing for box-to-box and internal links.
0.9 mm compact optical unit: For dense connectors, breakout assemblies and space-constrained internal equipment.
Optical fiber: Singlemode or multimode glass selected for the optical system.
Primary coating/buffer: Protects the glass and manages microbend sensitivity.
Strength member: Carries tensile load and separates installation stress from the fiber.
Protective jacket: Configured for abrasion, flex, cleanliness, flame or vacuum direction.
Optical termination: Ferrule, polish, alignment and strain relief are controlled as a process.
Optical system: Wavelength, source, receiver and allowable optical budget
Fiber type: Singlemode, multimode, simplex, duplex or multifiber
Length and routing: Installed length, bend radius and pull path
Mechanical load: Tension, crush, flex, vibration and connector retention
Environment: Temperature, cleanliness, vacuum, fluids or flame
Termination: Connector family, polish, breakout and inspection method
CM-FO-18-MM | Multimode · up to 100 Gb/s | 1.8 mm simplex with buffer, aramid strength and rugged jacket | ≤ 5.0 dB/km @ 850 nm · ≤ 3.0 dB/km @ 1300 nm | Avionics backbones, HD video and high-reliability box links
CM-FO-12-LW | Project-configured SM / OM1–OM5 | 1.2 mm lightweight simplex construction | ≤ 1.5 dB/km @ 1300 nm | Lightweight box links and dense airborne harnesses
CM-FO-09-COMPACT | Compact singlemode or multimode path | 0.9 mm optical unit with PFA/FEP/PEEK direction | 3.0 / 1.0 dB/km @ 850 / 1310 nm | Connector breakouts, internal equipment and confined links
Solution codes support early fiber-class, diameter and environment matching. Final part number, numerical aperture, wavelength, jacket, connectors and complete optical budget are confirmed to the system configuration.
Insertion loss and return loss where applicable
End-face inspection and polarity
Tensile, crush, bend and vibration
Environmental cycling with before/after optical comparison
High-speed equipment networks
EMI-sensitive avionics links
Cameras, sensors and instrumentation
Long-reach or isolated system links
Simplex and duplex optical connectors
Multifiber and ruggedized interfaces
Custom breakouts and hybrid assemblies
Optical performance depends on fiber class, wavelength, diameter, connector finish, length, bend state and contamination control; the complete link must be verified.