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High-Performance Aerospace Wire

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.

600 Vrms directionStable PD behaviorAbrasion and cut-through resistance
PRODUCT FAMILYPower Enablers
High-performance aerospace power wire construction
POWER / HPW / Representative construction · Final design follows the approved specification

01 / CONFIGURATION DIRECTIONS

Select a configuration from the application boundaries

These configurations establish a practical discussion starting point. The final product requires a controlled specification based on interface, length, installation and validation conditions.

01

Aircraft equipment wire

For airborne power and EWIS with mass, diameter and safety margin balanced.

02

Electric-aircraft wire

For higher system voltage, thermal load and electrification needs.

03

Defense-vehicle wire

Long-term stability against chemicals, humidity, abrasion and flame.

Match a solution direction to the link target

Solution codes support early technical discussions by aligning protocol, construction, link boundaries and application in one view.

SOLUTION CODEPROTOCOL / RATECONSTRUCTIONKEY BOUNDARYBEST FIT
POWER-HPW-01Aircraft equipment wireFor airborne power and EWIS with mass, diameter and safety margin balanced.600 Vrms directionMilitary and civil aircraft EWIS
POWER-HPW-02Electric-aircraft wireFor higher system voltage, thermal load and electrification needs.Stable PD behavioreVTOL and electric aviation
POWER-HPW-03Defense-vehicle wireLong-term stability against chemicals, humidity, abrasion and flame.Abrasion and cut-through resistanceDefense vehicle power

MODEL NOTEAmpacity, voltage and temperature rise must be defined with gauge, length, altitude, bundling, cooling and termination conditions.

02 / PERFORMANCE PARAMETERS

Product performance parameters

The following values describe current product performance boundaries, with the applicable model, construction or test condition retained.

PERFORMANCE METRICVALUECONFIGURATION / CONDITION
01Voltage rating600 Vrms

Sea-level withstand and PD condition

02Partial-discharge behaviorHigher PDIV / PDEV

Comparative direction versus common insulation

03Insulation materialEngineered fluoropolymer

Low-permittivity, hydrophobic, non-hydrolyzing direction

04Mechanical durabilityAbrasion & cut-through resistant

Material characteristic

05Material stabilityChemical inert · non-flammable

Material characteristic

06Qualification directionASTM D3032 · SAE AS29606 · SAE AS4373

Test standards

The 600 Vrms direction is based on sea-level voltage-withstand and partial-discharge performance; final capability depends on gauge and environment.

Technical referenceValues are confirmed against category, gauge, length and termination

03 / TYPICAL CONSTRUCTION

From functional core to terminated interface

LAYER 01

High-conductivity conductor

Gauge, stranding and plating are selected for resistance, flex and termination.

LAYER 02

Primary insulation

Thin-wall high-temperature material establishes voltage, PD and abrasion margin.

LAYER 03

Field or shield layer

Grading, shielding and return paths are added for high-voltage or EMI needs.

LAYER 04

Mechanical protection

Tapes, braid or jacket improve cut-through, wear and installation durability.

LAYER 05

Termination and strain relief

Crimp, solder, connector and thermal-cycle interfaces are controlled together.

04 / SELECTION & VALIDATION

Inputs needed to start a custom assessment

SELECTION ITEMINFORMATION TO CONFIRM
01Voltage and current

Continuous/peak voltage, current, frequency and partial-discharge boundary

02Gauge and drop

Length, conductor section, resistance and allowable voltage drop

03Thermal environment

Ambient, bundling, cooling and temperature rise

04Installation

Diameter, mass, bend radius, vibration and abrasion

05Material environment

Fluids, humidity, flame, smoke/toxicity or vacuum

06Termination

Terminal, crimp window, connector and strain relief

Typical applications

  • Military and civil aircraft EWIS
  • eVTOL and electric aviation
  • Defense vehicle power
  • High-reliability equipment wiring

Interfaces & delivery

  • Pigtail, terminal or crimp-contact delivery
  • Single-, two- or multicore feeder construction
  • Shielded or unshielded complete assembly
ENGINEERING NOTE

Ampacity, voltage and temperature rise must be defined with gauge, length, altitude, bundling, cooling and termination conditions.

Ready to define a controlled specification?

Bring us the interface, environment and validation requirements.

Yidong Telecom can build a sample direction and validation matrix around the cable construction, termination and system boundaries.

Submit requirement checklist