Conmoly | CM-POWER-HPW | High-Performance Aerospace Wire
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: Temperature-resistant, chemically inert and abrasion-resistant engineered fluoropolymer insulation supports stable high-voltage, lightweight and long-term material reliability in current and next-generation aircraft electrical systems.

The 600 Vrms direction is based on sea-level voltage-withstand and partial-discharge performance; final capability depends on gauge and environment.
Voltage rating: 600 Vrms | Sea-level withstand and PD condition
Partial-discharge behavior: Higher PDIV / PDEV | Comparative direction versus common insulation
Insulation material: Engineered fluoropolymer | Low-permittivity, hydrophobic, non-hydrolyzing direction
Mechanical durability: Abrasion & cut-through resistant | Material characteristic
Material stability: Chemical inert · non-flammable | Material characteristic
Qualification direction: ASTM D3032 · SAE AS29606 · SAE AS4373 | Test standards
Source: https://www.gore.com/products/high-performance-power-wire-aerospace-defense

Aircraft equipment wire: For airborne power and EWIS with mass, diameter and safety margin balanced.
Electric-aircraft wire: For higher system voltage, thermal load and electrification needs.
Defense-vehicle wire: Long-term stability against chemicals, humidity, abrasion and flame.
High-conductivity conductor: Gauge, stranding and plating are selected for resistance, flex and termination.
Primary insulation: Thin-wall high-temperature material establishes voltage, PD and abrasion margin.
Field or shield layer: Grading, shielding and return paths are added for high-voltage or EMI needs.
Mechanical protection: Tapes, braid or jacket improve cut-through, wear and installation durability.
Termination and strain relief: Crimp, solder, connector and thermal-cycle interfaces are controlled together.
Voltage and current: Continuous/peak voltage, current, frequency and partial-discharge boundary
Gauge and drop: Length, conductor section, resistance and allowable voltage drop
Thermal environment: Ambient, bundling, cooling and temperature rise
Installation: Diameter, mass, bend radius, vibration and abrasion
Material environment: Fluids, humidity, flame, smoke/toxicity or vacuum
Termination: Terminal, crimp window, connector and strain relief

Conductor resistance, voltage drop, hipot and insulation resistance
Partial discharge, breakdown and high-temperature electrical stability
Abrasion, cut-through, flex, tensile and vibration
Load temperature rise and post-cycle termination inspection
Military and civil aircraft EWIS
eVTOL and electric aviation
Defense vehicle power
High-reliability equipment wiring
Pigtail, terminal or crimp-contact delivery
Single-, two- or multicore feeder construction
Shielded or unshielded complete assembly
Ampacity, voltage and temperature rise must be defined with gauge, length, altitude, bundling, cooling and termination conditions.