
Type CSC Lightweight Space Cables
Reference configuration: ESCC 3901/025 lightweight GEO cable delivers 600 Vrms power and analog/low-frequency signals with smaller diameter, lower mass and tighter bending.
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CONMOLY / ENGINEERING & CONNECTIVITY
Reference configuration: 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.

Space Cables
CM-SPACE-ASW
Space Cables Type ASW
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.
GEO and LEO versions use different jacket and insulation systems; select the part number against the orbit environment.
Scroll the table horizontally to view all configuration conditions.
| Parameter | Reference value | Configuration / condition |
|---|---|---|
| Maximum operating voltage | 600 Vrms | Type ASW space wire |
| Temperature range | −200 to +200 °C | GEO / LEO range |
| GEO jacket | Conductive film | Antistatic construction |
| LEO jacket | Semi-conductive fluoropolymer | Antistatic / ATOX direction |
| Conductor | Silver-plated copper or copper | Version dependent |
| Wire gauges | 20 · 22 · 24 AWG | Standard part numbers |
Reference source: www.gore.com
| GEO conductive-film type | Conductive-film covering for moving geostationary-orbit systems. |
|---|---|
| LEO semiconductive type | Semiconductive fluoropolymer for low-orbit atomic oxygen. |
| 20–24 AWG single core | Standard gauge selected for resistance, mass and termination. |
| Space-grade conductor | Material, stranding and plating are selected for resistance, strength, flex and termination. |
|---|---|
| Low-outgassing insulation | Dielectric, thermal, vacuum-stability and processing requirements guide material selection. |
| Controlled functional unit | Single, twisted, shielded, coaxial or multicore signal geometry is formed. |
| Lightweight shield and cover | EMI, atomic oxygen, protection and mass are optimized together. |
| Termination and traceability | Connector, branch, strain relief, material lot and process records remain controlled. |
| Mission and orbit | LEO, GEO, deep space, launch phase and mission duration |
|---|---|
| Electrical function | Voltage, current, protocol, frequency, impedance and core count |
| Mass and space | Mass per meter, diameter, bend radius and route |
| Environment | Vacuum, thermal cycle, radiation, ATOX, vibration and shock |
| Harness interface | Connector, branch, lacing, ground and installation process |
| Verification level | Applicable ESCC/NASA documents, first article, lot and traceability |
Page values do not constitute mission qualification or approval. Applicable standards, lot screening and verification levels are confirmed per project.

Reference configuration: ESCC 3901/025 lightweight GEO cable delivers 600 Vrms power and analog/low-frequency signals with smaller diameter, lower mass and tighter bending.
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Reference configuration: ePTFE, PTFE and PFA combine in a chemical- and cut-through-resistant, low-springback wide-temperature space cable covering 12–30 AWG and multicore constructions.
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Reference configuration: ESCC 3901/026 lightweight LEO wire is up to 27% smaller and 47% lighter while delivering 600 Vrms power and analog/low-frequency signals.
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