Conmoly | CM-SPACE-LEW | Type LEW Low-Mass LEO 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: ESCC 3901/026 lightweight LEO wire is up to 27% smaller and 47% lighter while delivering 600 Vrms power and analog/low-frequency signals.

Diameter, mass and typical-mission savings are comparisons against peer ESCC cables.
Maximum operating voltage: 600 Vrms | Type LEW cable
Temperature range: −200 to +200 °C | Operating range
Diameter / weight reduction: Up to 27% / 47% | Versus ESCC 3901/012
Typical mission mass saving: Around 35% | Comparative estimate
Gauge range: 16–28 AWG | 21 variants
Specification: ESCC 3901/026 | ESA QPL
Source: https://www.gore.com/products/space-cables-type-lew

Single wire: Minimum-mass equipment and power connection.
Twisted pair: Balanced analog and low-frequency signals.
Shielded multicore cable: EMI control, compact routing 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

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
Manned/unmanned LEO spacecraft
Box-to-box analog signals
Power distribution
Mass-critical harnesses
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.