Mass & diameter
Assess per-meter mass and routing impact at full-harness scale.
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SPACE / 06
Space Cables
Supporting spacecraft interconnects through materials, mass and verifiability
Design directions for spacecraft data, power and RF interconnects, with emphasis on low mass, vacuum material behavior, thermal cycling, vibration, routing constraints and lot traceability.
LightweightLow-outgassing design directionHigh-reliability interconnect
TYPICAL APPLICATIONSSpacecraft data, power, RF and internal harness interconnects
01 / PRODUCT OVERVIEW
Define the construction from system constraints
This information supports product direction and early technical discussions. Yidong Telecom defines final materials, dimensions and manufacturing around the actual interface, environment and validation target.
Vacuum-material direction
Consider outgassing, volatiles, contamination control and traceability.
Thermomechanical stability
Evaluate thermal cycling, vibration and assembly stress.
Verification & traceability
Build evidence from material lots through process records and lot tests.
02 / PRODUCT TYPES
Series scope and selection direction
Each type must be further defined by protocol, length, installation and environmental conditions. A category name is not a fixed specification.
Space Cables Type ASW
Lightweight space-wire direction tailored around conductors, thin-wall insulation, temperature and assembly.
View specific product ↗Space Cables Type CSC
Controlled signal or communication construction with cores and shielding defined by system interface.
View specific product ↗Space Cables Type CSWL
Lightweight multicore or shielded direction linked to harness processing and environmental validation.
View specific product ↗Space Cables Type LEW
Lightweight equipment wiring direction focused on diameter, mass and conductor mechanical reliability.
View specific product ↗Space Cables Type SPM
Specialized mission or platform interconnect direction defined by electrical, mechanical and interface conditions.
View specific product ↗Spaceflight Microwave RF Assemblies
Low-loss coax, connectors, strain relief and thermomechanical requirements assessed as one assembly.
View specific product ↗SpaceWire
SpaceWire-class differential links focused on impedance, delay, crosstalk, shielding and mass.
View specific product ↗03 / ENGINEERING DESIGN
Critical design goals
Typical construction path
Lightweight conductor
Material, stranding and plating selected for resistance, strength, flex and termination.
Space material system
Insulation screened for dielectric, thermal, vacuum and processing requirements.
Controlled signal unit
Twisted pair, quad, coaxial or multicore geometry.
Shield & lightweight covering
EMI, protection and mass balanced across shields, tapes and jackets.
Harness & termination
Connectors, lacing, branching, strain relief and spacecraft installation validated together.
04 / SELECTION & VALIDATION
Inputs needed to start solution assessment
01
Mission phase and applicable standards
02
Protocol, frequency, impedance, voltage and current
03
Length, mass budget and routing
04
Vacuum, thermal cycling, radiation and contamination controls
05
Vibration, shock and termination
06
Material lots, samples and traceability
IMPORTANT NOTE
This page describes space-product design directions and is not a qualification, screening or mission-approval statement. Applicable standards and validation levels are confirmed per project.
Ready to turn a product direction into a controlled specification?
Start an engineering assessment with your application boundaries.
Prepare protocol, electrical, mechanical, environmental, interface and validation requirements so we can define the material, construction and sample-validation path.
Return to requirement checklist ↗