On-Board Computers (OBC)

48 On-Board Computers (OBC) for Space Applications from 26 manufacturers listed on SatNow

On-Board Computers (OBC) for space applications from multiple manufacturers are listed on SATNow. Use the filters to select products based on your requirement. View product details, download datasheets, compare products, get quotes and pricing for matching products. SATNow has compiled this list of products specifically for Space and Satellite Applications.

Description:Full Redundant On-Board Computer with reconfiguration GPS Receiver
Satellite Type:
SmallSat
Orbit:
LEO
Mass:
3.5 Kg
Voltage:
22 to 38 V, 5 V (Secondary)
Power Consumption:
20 to 50 W
Altitude Stabilization Component:
Magnetorquers
Interface:
Ethernet, SpaceWire, RS-422, Pcle
Space Heritage:
Yes
more info
Description:On Board Flight Computer is a highly Integrated Nano Satellite and CubeSat
Satellite Type:
NanoSat
Altitude Stabilization Component:
Magnetometer, Gyroscope
Interface:
CAN, SPI, I2C, UART, SPI, USB, USART
Space Heritage:
Yes
more info
Description:SmartFusion 2 SoC With including Cortex-M3 processor @ 50 MHz delivering 62.5 DMIPS
Satellite Type:
NanoSat
Orbit:
LEO
Mass:
0.0619 Kg
Voltage:
3.3 V
Power Consumption:
0.4 to 1 W
Radiation:
20 Krad
Interface:
I2C, SPI, UART, PCle, CAN, LVDS, RS-485
Space Heritage:
Yes
more info
Description:Auxiliary Processor Operate via a Linux Operation System
Orbit:
LEO
Mass:
0.87 Kg
Interface:
RS-422, PCle
Space Heritage:
Yes
more info
Description:Gyroscope And Magnetometer Attitude stabilization System Represents a Raspberry-Pi Compute
Satellite Type:
CubeSat
Mass:
0.055 Kg
Voltage:
5 to 5.14 V
Current:
200 mA (Simple Payloads), Up to 650 mA (External)
Power Consumption:
0.015 to 0.9 W
Altitude Stabilization Component:
Magnetometer, Gyroscope
Interface:
CAN, SPI, I2C, USB, UART
Space Heritage:
Yes
more info
Description:Low Power Flight Computer Designs For Microsatellite Projects Low Earth Orbit Spacecrafts
Satellite Type:
MicroSat
Orbit:
LEO
Mass:
0.35 Kg
Voltage:
22 to 34 V
Power Consumption:
5 W
Radiation:
15 Krad
Interface:
RS-422, PCle, CAN, UART, SpaceWire
Space Heritage:
Yes
more info
Description:Rugged Automotive Grade Components Or General Application On Mini And Micro Satellites
Satellite Type:
MiniSat, MicroSat
Mass:
0.15 Kg
Voltage:
8 to 12 V
Current:
50 to 150 mA
Interface:
CAN, RS-422, Pcle
more info
Description:Space Micro’s latest Image Processing Computer UltraScale FPGAs in a VPX backplane
Satellite Type:
CubeSat
Radiation:
100 Krad
Interface:
LVDS, RS-422, PCle, USB
Space Heritage:
Yes
more info
Description:The Modular, Plug & Play And Protective On-Board Computer
Satellite Type:
CubeSat
Mass:
0.025 Kg
Voltage:
3.3 to 5 V
Power Consumption:
0.1 W
Radiation:
20 Krad
Altitude Stabilization Component:
Magnetometer, Gyroscope / ACC
Interface:
I2C, RS-485, UART, CAN, SPI, PWM
Space Heritage:
Yes
more info
Description:ISIS On Board Computer 400 MHz, Power Efficient ARM9 Processor
Satellite Type:
CubeSat
Mass:
0.094 Kg (Mainboard), 0.1 Kg (EM daughter board)
Voltage:
3.3 V
Power Consumption:
0.4 W
Interface:
I2C, SPI, UART, RS-422, PCle, RS-485, RS-232, USB
Space Heritage:
Yes
more info


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