Conmoly | CM-SPACE-CSWL | Type CSWL Wide-Temperature Space Cables
Shenzhen Xinju New Materials Technology Co., Ltd.
https://conmoly.com

Selection reference; third-party published figures are not Conmoly guaranteed specifications or certifications. Final specifications require configuration review. Images illustrate product form.
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.

Type CSWL has multiple core-count and gauge variants; the table shows family-wide environmental and voltage ranges.
Maximum operating voltage: 600 Vrms | Type CSWL cable
Temperature range: −200 to +200 °C | Operating range
Gauge range: 12–30 AWG | 64 variants
Core count: 1–4 cores | Example standard constructions
Jacket: Expanded PTFE + PFA | Material system
Specification: ESCC 3901/024 | Ordering designation
Source: https://www.gore.com/products/space-cables-type-cswl

Single-core space wire: 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.
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

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
Traditional spacecraft harnesses
Power and low-frequency signals
Extreme-temperature equipment
Compact low-springback routing
Single, multicore or shielded space cable
Space connector and lightweight harness
Fixed-length assembly, branch or pigtail
Page values do not constitute mission qualification or approval. Applicable standards, lot screening and verification levels are confirmed per project.