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Type CSWL Wide-Temperature Space Cables
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.
Product form illustration · Final construction depends on configuration
Space Cables
CM-SPACE-CSWL
Space Cables Type CSWL
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.
Type CSWL has multiple core-count and gauge variants; the table shows family-wide environmental and voltage ranges.
Scroll the table horizontally to view all configuration conditions.
For power and low-frequency equipment interconnects.
2–4 core cable
Multiple power or signal paths within one jacket.
64 standard variants
Core count and gauge selected under ESCC 3901/024.
Cable construction
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.
Selection checklist
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
Applications
Traditional spacecraft harnesses
Power and low-frequency signals
Extreme-temperature equipment
Compact low-springback routing
Interfaces & termination
Single, multicore or shielded space cable
Space connector and lightweight harness
Fixed-length assembly, branch or pigtail
Project validation checklist
Electrical baseline before and after thermal cycling
Vibration, shock, flex and termination retention
Mission-defined outgassing, radiation or atomic-oxygen evidence
First article, lot consistency and material/process traceability
Page values do not constitute mission qualification or approval. Applicable standards, lot screening and verification levels are confirmed per project.
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.
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.
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.