CAVU Aerospace UK

Implementing a Radiation-Tolerant OBC with 6×1Gb Ethernet Using PolarFire SoC FPGA

As spacecraft architectures evolve toward distributed, high-throughput systems, the On-Board Computer (OBC) is no longer just a controller—it is the central data router, processor, and reliability backbone of the mission.

The OBC-Hypr-Polar, developed by Cavu Aerospace UK, is designed around this philosophy. By combining a PolarFire SoC FPGA with six 1Gb Ethernet interfaces and a high-reliability power subsystem using Glenair Micro-D connectors, the system achieves both performance and mission-grade robustness.

The OBC-Hypr-Polar is built around the Microchip Technology PolarFire SoC FPGA, which integrates:

  • Multi-core RISC-V processors for software-defined control
  • FPGA fabric for deterministic, parallel data handling
  • Low-power architecture ideal for space platforms
  • Radiation-tolerant design suitable for LEO and deep-space missions

This hybrid approach allows:

  • Hardware-accelerated Ethernet switching and packet handling
  • Real-time payload interfacing
  • Software flexibility for mission updates

High-Speed Networking: 6× Independent 1Gb Ethernet Ports

The OBC-Hypr-Polar provides six isolated Gigabit Ethernet interfaces, enabling:

Distributed Spacecraft Architectures

Each subsystem (payload, ADCS, communications, storage) can operate as a network node, reducing centralized bottlenecks.

Redundancy and Fault Tolerance

Multiple Ethernet links allow:

  • Cross-strapping between subsystems
  • Ring or mesh redundancy
  • Graceful degradation under failure

FPGA-Based Networking

Using the PolarFire FPGA fabric, the OBC can implement:

  • Deterministic Ethernet switching
  • Custom packet routing
  • Time-Sensitive Networking (TSN)

Multi-Interface Support

Beyond Ethernet, the system integrates:

  • LVDS for high-speed sensor interfaces
  • Serial I/O for legacy subsystems and housekeeping
  • ADC interface for analog telemetry acquisition
  • JTAG-USB debug for development and diagnostics

This ensures compatibility across a wide range of spacecraft subsystems.

Power Subsystem: FMEA-Driven Reliability Engineering

A comprehensive Failure Modes and Effects Analysis (FMEA) identified the power subsystem as the highest-risk element in the OBC.

Failures in power delivery can result in:

  • Complete system shutdown
  • FPGA latch-up or reset
  • Data corruption or mission loss

To mitigate these risks, the OBC-Hypr-Polar incorporates:

  1. Radiation-Tolerant DC/DC Conversion
    • Stable operation across temperature extremes
    • Protection against transients and single-event effects
    • High efficiency to reduce thermal load
  1. High-Reliability Power Interconnect

Glenair Micro-D Connector (IGMPM2-B112R-CBRT-SU-.109)

The OBC uses a Glenair Micro-D combo connector, specifically designed for power and signal integration in harsh environments.

Why This Connector Matters

a) High Current Capability in Compact Form

  • Approximately 13A per contact
  • Enables reliable power delivery without bulky connectors
  • Ideal for compact spacecraft avionics

b) Combo Micro-D Architecture

The connector combines:

  • Power contacts
  • Signal contacts
  • Compact Micro-D footprint

This reduces:

  • Connector count
  • Harness complexity
  • Potential failure points

c) Ruggedized PCB Mount Design

  • Right-angle PCB mounting with encapsulation support
  • Epoxy-sealed contacts improve:
    • Resistance to vibration
    • Resistance to thermal cycling
  • Ensures mechanical integrity during launch conditions

d) Space-Grade Materials

  • Beryllium copper contacts for high conductivity and durability
  • Gold plating for corrosion resistance and low contact resistance
  • Aluminum alloy shell with protective finish for strength and EMI shielding

e) Wide Operating Temperature Range

  • Typically −55°C to +150°C
  • Suitable for:
    • Low Earth Orbit thermal cycling
    • Deep space missions

f) Mechanical Reliability

  • High mating cycle durability
  • Secure locking mechanism
  • Strong resistance to vibration and shock

Engineering Impact of Using Glenair Power Connectors

Improved Reliability

By reducing connector-related failure modes such as:

  • Intermittent contact
  • Mechanical wear
  • Thermal degradation

Reduced System Risk

The power interface becomes:

  • Mechanically stable
  • Electrically robust
  • Environmentally resilient

Optimized Mass and Volume

Compared to traditional circular connectors:

  • Smaller footprint
  • Lower mass

Higher integration density

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Mechanical and System Integration

The connector layout of the OBC-Hypr-Polar is designed for:

  • Clear separation of:
    • Power
    • Data
    • Debug interfaces
  • Simplified harness routing
  • Reduced electromagnetic interference between high-speed and power lines

Why PolarFire SoC and Glenair is a Strong Combination

Aspect

PolarFire SoC FPGA

Glenair Micro-D Connector

Reliability

Radiation-tolerant logic

Rugged mechanical and electrical interface

Power Efficiency

Low-power FPGA fabric

High-current, low-loss connection

Integration

Multi-function SoC

Power and signal in a single connector

Space Suitability

Single-event upset resilient design

Proven aerospace heritage