CONMOLY / ENGINEERING & CONNECTIVITY
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.
Power Enablers
CM-POWER-HPW
High Performance Aerospace Wire
Reference configurations only; specifications and certifications require confirmation.
Selection reference. Published third-party figures below describe specific reference configurations; they are not Conmoly guaranteed values or certifications. Confirm the final construction and test requirements with engineering.
The 600 Vrms direction is based on sea-level voltage-withstand and partial-discharge performance; final capability depends on gauge and environment.
Scroll the table horizontally to view all configuration conditions.
| Parameter | Reference value | Configuration / condition |
|---|---|---|
| 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 |
Reference source: www.gore.com
| 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 |
Ampacity, voltage and temperature rise must be defined with gauge, length, altitude, bundling, cooling and termination conditions.
Reference configuration: Low-loss engineered fluoropolymer film for aerospace power electronics and harsh-environment capacitors, maintaining voltage and capacitance stability under heat, field stress and long energized duty.
View specifications
Reference configuration: Engineered fluoropolymer insulation protects copper windings and maintains insulation resistance and breakdown performance in high temperature, high pressure, oil and hydrolysis environments.
View specifications
Reference configuration: High-voltage, wide-temperature, low-springback feeder paths for aircraft main power and electrification systems, controlling partial discharge, thermal aging, abrasion and constrained routing.
View specifications