CAVU Aerospace UK Ltd

OBC CUBE POLAROBC CUBE POLAR

The OBC-Polar is a cutting-edge onboard computer specifically designed for Cubesat missions. Leveraging the powerful and reliable Microchip PolarFire SoC FPGA technology, this Cubesat OBC provides exceptional performance and versatility for space applications. Whether your mission involves scientific research, Earth observation, or commercial satellite deployment, the OBC-Polar ensures optimal performance and reliability in the harsh conditions of space.

SEU Immune PolarFire SoC FPGA Platform

More Than 4000DMIPS Processing Power

Large RAM with ECC Support

Multiple High speed CameraLink interface

FrameGrabber

POLAR EDGEPOLAR EDGE

The Polar Edge is a cutting-edge onboard super computer powered by Artificial Intelligence specifically designed for Cubesat missions. Leveraging the powerful and reliable Microchip PolarFire SoC FPGA technology & NVIDIA Jetson Orin, this Cubesat OBC provides exceptional performance and versatility for space applications. Whether your mission involves scientific research, Earth observation, or commercial satellite deployment, the Polar Edge ensures optimal performance and reliability in the harsh conditions of space.

SEU Immune PolarFire SoC FPGA Platform &

NVIDIA Jetson Orin OnBoard

Super Flight Computer In-Orbit AI

OBC POLAROBC POLAR

The OBC-Polar is a cutting-edge onboard computer specifically designed for Cubesat missions. Leveraging the powerful and reliable Microchip PolarFire SoC FPGA technology, this Cubesat OBC provides exceptional performance and versatility for space applications. Whether your mission involves scientific research, Earth observation, or commercial satellite deployment, the OBC-Polar ensures optimal performance and reliability in the harsh conditions of space.

SEU Immune PolarFire SoC FPGA Platform

More Than 4000DMIPS Processing Power

Large RAM with ECC Support 

CDH-FSCDH-FS

CDH-FS represents the pinnacle of on-board computer systems, featuring a fully redundant FPGA-based architecture designed to guarantee continuous operation. With a backup processor that seamlessly engages upon primary processor failure, this system is not just reliable; it’s essential for critical missions. Engineered to resist severe space conditions like radiation and cosmic rays, it leverages the efficiency and SEU immunity of Microchip/Microsemi SmartFusion2 and ProASIC3 Flash-based FPGAs.

Dual Cold/Hot Redundant OBC Modules

Dual Cold/Hot Redundant ADC/DAC Modules

Double Hot Redundant ADC Converters

Advanced Supervisor & Health Monitoring Module

TCUTCU

Thermal Control Unit offers efficient thermal management for satellite systems, ensuring reliable performance in space. Using FPGA-based control and radiation mitigation techniques, it optimizes power use for long-duration missions with customizable sensor inputs and heater channels.

Supports 110 sensor inputs, 50 heaters output

FPGA-based control with SEU mitigation

Real-time thermal monitoring 

Adjustment Interface to Thermistors, RTD, etc.

Fully Customizable

FG1FG1

The FG-1 is a state-of-the-art Cubesat satellite board, specifically designed for capturing high-quality images from a CameraLink camera in a Cubesat satellite. This device embodies the latest advancements in space technology, ensuring optimal performance even in the harsh conditions of space.

SATELLITE CAMERASATELLITE CAMERA

Flight proven highly reliable optical payload, for capturing high-resolution images from the ground surface and atmospheric phenomena. The s.LDU.345 has been designed to be implementable in a standard CubeSat structure together with other subsystems to allow low-cost Earth observation.

Camera- Aperture Size: 60 mm
Data Interface: LVDS + RS422 + Ethernet
Data Transmission Interface: UART RS485 @6.25
Image format: RAW + JPEG
Adjustable parameters: Integration Time , Frame Rate , Gain, Black Level

SOLAR ARRAY SOLAR ARRAY

Modular solar panels (RAMS, Assembling Modular Solar-panel) with a thin carbon fiber – aluminum honeycomb board as a module structure, combined with carbon fiber – aluminum honeycomb frame structure, through a number of modules and frame assembly, you can achieve solar panels Of the rapid assembly and integration, both as a spacecraft solar array plate can also be used as a development board, the output power range of 15W ~ 530W.

CAVU AEROSPACE UK, ESA Entity No.: 1000042906

Our core business is Command & Data Handling. We have series of flight proven onboard computers (OBCs) for satellite and launch vehicles. With several projects delivered to global aerospace enterprises including space agencies, satellite companies & launch firms since 2016, our cutting-edge technology for Flight Computers, Thermal Control, Payload Interface, CameraLink products is complemented by our extensive expertise in aerospace systems and precision manufacturing. This includes the development of rugged hardware, efficient software solutions, and seamless integration of all system components to ensure that each satellite operates effectively even in the harshest space environments.

MODULES IN ORBITMODULES IN ORBIT

SATELLITES SUPPLIEDSATELLITES SUPPLIED

TB DATA DOWNLINKEDTB DATA DOWNLINKED

Flight Proven Products OnBoard ComputersEdge Super ComputersThermal Control UnitPayload Interface UnitInstrument Control UnitSatellite & Rockets CameraSolar Arrays

CLIENTS & PARTNERS CLIENTS & PARTNERS

CLIENTS & PARTNERS CLIENTS & PARTNERS