CAVU Aerospace UK

Compare OBC-104 & Cube-Polar

We offer two primary On-Board Computer platforms in the CubeSat form factor: OBC-104 and OBC-Cube-Polar. Both platforms are technically competitive in the market and are manufactured in series production to improve commercial attractiveness by reducing lead times and overall costs. Each OBC is supported by open-source software, BSPs, and a mature software ecosystem. The following comparison is intended to help mission designers select the most suitable OBC based on their mission requirements.

 

Feature

OBC-Cube-104

OBC-Cube-Polar

Platform

SmartFusion2 Flash FPGA

(ARM Cortex-M3)

Microchip PolarFire SoC FPGA

(Quad RISC-V + monitor core)

Form Factor

CubeSat

CubeSat

Target

Budget / standard CubeSat missions

Advanced & compute-intensive missions

SW Support

Bare-metal/RTOS (via Cortex-M3)

Linux, RTOS (e.g. Linux, FreeBSD, Integrity) CAVU Aerospace

 

Processing Power

OBC-Cube-104

  • ARM Cortex-M3 (inside SmartFusion2 FPGA fabric).
  • Up to ~150 DMIPS @ ~128 MHz (max ~166 MHz).
  • Suitable for typical command & data handling, housekeeping, and lightweight payload processing. CAVU Aerospace

OBC-Cube-Polar

  • Quad 64-bit RISC-V cores @ 660 MHz each — >4000 DMIPS total.
  • Includes a monitoring core and optional soft cores.
  • Orders of magnitude higher CPU performance than Cube-104.
  • Designed to run full OS (e.g., Linux) for complex applications. CAVU Aerospace

👉 Which suits which?

  • Cube-104: Adequate for missions with basic CDH, simple payload control, ADCS demo missions, or low data-rate science.
  • Cube-Polar: Best for missions requiring significant on-board data processing, complex payload control, ML/AI, real-time image processing, or advanced autonomy.

 

Interface Capability

OBC-Cube-104 Interfaces

  • Digital I/O: ~20–60.
  • ADC: 8 channels.
  • Serial: CAN2.0×4, RS422×4, RS485×4, RS232×2.
  • I2C×2, SPI×2.
  • SpaceWire×2, optional CameraLink.CAVU Aerospace

OBC-Cube-Polar Interfaces

Typical interfaces (from datasheets / catalog listings):

  • UART, SPI, I2C.
  • SpaceWire.
  • LVDS.
  • USB 2.0.
  • Gigabit Ethernet (GigE).
  • CAN2.0B, RS422, RS232.
  • ADC (unspecified channels, but large connectivity).
  • PCIe support via daughter-card/SerDes.satsearch.co

👉 Comparison:

  • Cube-104: Strong on basic serial and legacy buses, suitable for comms & AOCS.
  • Cube-Polar: Broader, higher bandwidth interfaces including USB/GigE/PCIe and more flexible payload connectivity — suitable for data-heavy instruments like imagers, LiDAR, or high-rate science.

 

Power Consumption

Model

Typical Power Consumption

OBC-Cube-104

~1 W – 2 W CAVU Aerospace

OBC-Cube-Polar

~1.5 W – 6 W (catalog / dependent on config) satsearch.co

👉 Notes:

  • Cube-104’s low power envelope makes it ideal for very power-limited missions or smaller CubeSats (1U/2U).
  • Cube-Polar consumes more (higher compute cost) but still within typical CubeSat power budgets — fits missions with larger power availability (e.g., 6U+ or dedicated Earth observation).

 

Memory & Storage

OBC-Cube-104

  • MRAM/FRAM with ECC; up to ~192 Gbit NAND Flash.
  • Up to ~112 Mbit RAM + 512 KB eNVM. CAVU Aerospace

OBC-Cube-Polar

  • Large RAM with ECC (2 GB or 4 GB options).
  • eMMC Flash (~64 GB), QSPI (~1 Gb), FRAM/MRAM, microSD slot.
  • Fully modern storage suitable for large datasets. CAVU Aerospace

👉 Cube-Polar is much better suited for data-intensive storage & caching (e.g., onboard preprocessing of images, science data buffering prior to downlink).

 

Operational & Software Support

  • Cube-104: Suitable for bare-metal or lightweight RTOS (e.g., FreeRTOS). Best for well-controlled deterministic tasks.
  • Cube-Polar: Supports full OS environments (Linux, Integrity, FreeBSD), enabling advanced scheduling, networking, filesystem support, and complex autonomy. CAVU Aerospace

OBC-Cube-104

Best for:

  • Standard CubeSat CDH (Command/Control & Housekeeping)
  • AOCS & comms handling
  • Low data rate research payloads
  • Power-constrained missions (<2 W budget)
  • Smaller form-factor CubeSats (1U/2U)

Not ideal for:

  • On-board image processing
  • High-rate data handling
  • Full OS running
  • Large science payloads

OBC-Cube-Polar

Best for:

  • High-bandwidth instruments (cameras, spectrometers, LiDAR)
  • Real-time image/data processing
  • On-board autonomy / AI algorithms
  • Scientific missions with high throughput
  • Secondary payload processing

Considerations:

  • Requires careful power budgeting (1.5 W to 6 W).
  • Larger memory and interfaces benefit data-heavy missions.

 

In Brief:

OBC-Cube-104 excels where simplicity, low power, and legacy interfaces are priorities.
OBC-Cube-Polar excels where computing performance, modern interfaces, and advanced software ecosystems are critical.

Mission Type

Recommended OBC

Basic CDH / house-keeping

OBC-Cube-104

AOCS & communication

OBC-Cube-104 / mid-range CubePolar

Low-rate payloads

Cube-104

High rate cameras / EO

OBC-Cube-Polar

Onboard processing / autonomy

OBC-Cube-Polar

Big data storage & buffering

OBC-Cube-Polar

 

OBC Onboard Computer OBC-104 Cube-Polar Microchip