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SpaceWire Data Cables

LVDS serial point-to-point links carry bidirectional data up to 400 Mbps with low crosstalk, loss and skew plus lightweight shielding for critical spacecraft interconnects.

400 Mbps≤150 ps/m intra-pair skew10+ MRad
PRODUCT FAMILYSpace Cables
SpaceWire high-speed differential space cable construction
SPACE / SPACEWIRE / Representative construction · Final design follows the approved specification

01 / CONFIGURATION DIRECTIONS

Select a configuration from the application boundaries

These configurations establish a practical discussion starting point. The final product requires a controlled specification based on interface, length, installation and validation conditions.

01

26 AWG SpaceWire

Balances link loss, mechanical strength and termination.

02

28 AWG lightweight type

Reduces diameter and mass for dense routing.

03

Terminated assembly

Connector, length and shield grounding form the complete channel.

Match a solution direction to the link target

Solution codes support early technical discussions by aligning protocol, construction, link boundaries and application in one view.

SOLUTION CODEPROTOCOL / RATECONSTRUCTIONKEY BOUNDARYBEST FIT
SPACE-SPACEWIRE-0126 AWG SpaceWireBalances link loss, mechanical strength and termination.400 MbpsHigh-resolution cameras
SPACE-SPACEWIRE-0228 AWG lightweight typeReduces diameter and mass for dense routing.≤150 ps/m intra-pair skewRadar and sensor equipment
SPACE-SPACEWIRE-03Terminated assemblyConnector, length and shield grounding form the complete channel.10+ MRadMemory and telemetry subsystems

MODEL NOTEPage values do not constitute mission qualification or approval. Applicable standards, lot screening and verification levels are confirmed per project.

02 / PERFORMANCE PARAMETERS

Product performance parameters

The following values describe current product performance boundaries, with the applicable model, construction or test condition retained.

PERFORMANCE METRICVALUECONFIGURATION / CONDITION
01Data rate400 Mbps

Bidirectional LVDS link

02Maximum operating voltage200 Vrms

Traditional-space configuration

03Time delay4.30 ns/m

Pair

04Intra-pair skew≤ 150 ps/m

Specification limit

05Dielectric withstand1400 Vrms

Conductor-conductor/shield

06Temperature / radiation−200 to +180 °C · 10+ MRad

Traditional-space configuration

07Vacuum stabilityVCM < 0.1% · TML < 1.0%

ASTM 595 / ECSS-Q-70-02

Values apply to the traditional-space SpaceWire configuration; choose 26 or 28 AWG against link and mass budgets.

Technical referenceValues are confirmed against category, gauge, length and termination

03 / TYPICAL CONSTRUCTION

From functional core to terminated interface

LAYER 01

Space-grade conductor

Material, stranding and plating are selected for resistance, strength, flex and termination.

LAYER 02

Low-outgassing insulation

Dielectric, thermal, vacuum-stability and processing requirements guide material selection.

LAYER 03

Controlled functional unit

Single, twisted, shielded, coaxial or multicore signal geometry is formed.

LAYER 04

Lightweight shield and cover

EMI, atomic oxygen, protection and mass are optimized together.

LAYER 05

Termination and traceability

Connector, branch, strain relief, material lot and process records remain controlled.

04 / SELECTION & VALIDATION

Inputs needed to start a custom assessment

SELECTION ITEMINFORMATION TO CONFIRM
01Mission and orbit

LEO, GEO, deep space, launch phase and mission duration

02Electrical function

Voltage, current, protocol, frequency, impedance and core count

03Mass and space

Mass per meter, diameter, bend radius and route

04Environment

Vacuum, thermal cycle, radiation, ATOX, vibration and shock

05Harness interface

Connector, branch, lacing, ground and installation process

06Verification level

Applicable ESCC/NASA documents, first article, lot and traceability

Typical applications

  • High-resolution cameras
  • Radar and sensor equipment
  • Memory and telemetry subsystems
  • Spacecraft high-speed backbone

Interfaces & delivery

  • Single, multicore or shielded space cable
  • Space connector and lightweight harness
  • Fixed-length assembly, branch or pigtail
ENGINEERING NOTE

Page values do not constitute mission qualification or approval. Applicable standards, lot screening and verification levels are confirmed per project.

Ready to define a controlled specification?

Bring us the interface, environment and validation requirements.

Yidong Telecom can build a sample direction and validation matrix around the cable construction, termination and system boundaries.

Submit requirement checklist