Home/Product families/Space Cables/Type ASW Anti-Static Space Wire

SPACE / ASW / 01

Type ASW Anti-Static Space Wire

Conductive or semi-conductive covers continuously drain static charge and provide lightweight, flexible, atomic-oxygen-resistant 600 Vrms power interconnects for moving LEO and GEO systems.

600 Vrms−200 to +200 °CGEO/LEO antistatic cover
PRODUCT FAMILYSpace Cables
Type ASW anti-static space wire construction
SPACE / ASW / 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

GEO conductive-film type

Conductive-film covering for moving geostationary-orbit systems.

02

LEO semiconductive type

Semiconductive fluoropolymer for low-orbit atomic oxygen.

03

20–24 AWG single core

Standard gauge selected for resistance, mass and termination.

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
SPACE-ASW-01GEO conductive-film typeConductive-film covering for moving geostationary-orbit systems.600 VrmsIon thrusters
SPACE-ASW-02LEO semiconductive typeSemiconductive fluoropolymer for low-orbit atomic oxygen.−200 to +200 °CSolar-array wiring
SPACE-ASW-0320–24 AWG single coreStandard gauge selected for resistance, mass and termination.GEO/LEO antistatic coverStationary plasma thrusters

MODEL NOTEPage values do not constitute mission qualification or approval. Applicable standards, lot screening and verification levels are confirmed per project.

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
01Maximum operating voltage600 Vrms

Type ASW space wire

02Temperature range−200 to +200 °C

GEO / LEO range

03GEO jacketConductive film

Antistatic construction

04LEO jacketSemi-conductive fluoropolymer

Antistatic / ATOX direction

05ConductorSilver-plated copper or copper

Version dependent

06Wire gauges20 · 22 · 24 AWG

Standard part numbers

GEO and LEO versions use different jacket and insulation systems; select the part number against the orbit environment.

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

03 / TYPICAL CONSTRUCTION

From functional core to terminated interface

LAYER 01

Space-grade conductor

Material, stranding and plating are selected for resistance, strength, flex and termination.

LAYER 02

Low-outgassing insulation

Dielectric, thermal, vacuum-stability and processing requirements guide material selection.

LAYER 03

Controlled functional unit

Single, twisted, shielded, coaxial or multicore signal geometry is formed.

LAYER 04

Lightweight shield and cover

EMI, atomic oxygen, protection and mass are optimized together.

LAYER 05

Termination and traceability

Connector, branch, strain relief, material lot and process records remain controlled.

04 / SELECTION & VALIDATION

Inputs needed to start a custom assessment

SELECTION ITEMINFORMATION TO CONFIRM
01Mission and orbit

LEO, GEO, deep space, launch phase and mission duration

02Electrical function

Voltage, current, protocol, frequency, impedance and core count

03Mass and space

Mass per meter, diameter, bend radius and route

04Environment

Vacuum, thermal cycle, radiation, ATOX, vibration and shock

05Harness interface

Connector, branch, lacing, ground and installation process

06Verification level

Applicable ESCC/NASA documents, first article, lot and traceability

Typical applications

  • Ion thrusters
  • Solar-array wiring
  • Stationary plasma thrusters
  • LEO/GEO moving mechanisms

Interfaces & delivery

  • Single, multicore or shielded space cable
  • Space connector and lightweight harness
  • Fixed-length assembly, branch or pigtail
ENGINEERING NOTE

Page values do not constitute mission qualification or approval. Applicable standards, lot screening and verification levels are confirmed per project.

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