Satellite On-Board Computers (OBC)

9 Satellite On-Board Computers (OBC) from 4 Manufacturers meet your specification.
Selected Filters Reset All
  • Manufacturers: SkyLabs d.o.o., STM Defense International, Dragonfly Aerospace, SPUTNIX
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
SKU:NANOobc-2
Satellite Type:
SmallSat, NanoSat, MicroSat
Mass:
0.055 Kg
Voltage:
5 V
Power Consumption:
1 W (peek), 0.9 W (idle mode)
Interface:
SpaceWire, RS-422, PCle, RS-485
Space Heritage:
Yes
more info
SKU:NANOSATPRO
Satellite Type:
MicroSat, NanoSat
Orbit:
LEO
Mass:
0.1 Kg
Voltage:
4.5 to 5.5 V
Radiation:
30 Krad (Si)
Interface:
UART, I2C, SPI, CAN, RS-485, PCle
more info
Description:High Reliability, Low-Power Flight Computer with Integrated AOCS Interface and Controller for Low Earth Orbit Spacecraft
Orbit:
LEO
Mass:
0.35 Kg
Voltage:
24 to 32 V
Power Consumption:
5 W
Interface:
CAN, SpaceWire, RS-422, RS-485
more info
SKU:MICROSATPRO
Satellite Type:
MicroSat, NanoSat
Orbit:
LEO
Mass:
0.28 Kg
Voltage:
3.3 to 5.5 V
Power Consumption:
3 W
Radiation:
30 Krad
Interface:
SpaceWire, RS-422, PCle, RS-485, CAN, SPI, I2C, UART, USB
more info
SKU:SX-SBOX-OBC-01
Satellite Type:
MicroSat
Mass:
0.86 Kg
Voltage:
22 to 34 V
Power Consumption:
Up to 10 W
Altitude Stabilization Component:
Gyro, Magnetometer, Sensors
Interface:
CAN
Space Heritage:
Yes
more info
SKU:NANOhpm-obc
Orbit:
LEO
Mass:
0.06 Kg
Voltage:
5 V
Power Consumption:
5 W
Radiation:
300 Krad
Interface:
LVDS, RS-422, PCle, RS-485, CAN, SPI, I2C, UART, USB
Space Heritage:
Yes
more info
SKU:SXC-MB-04-ADC
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:Flat and flexible architecture On Board Computer with CAN bus interconnect
Satellite Type:
CubeSat
Mass:
0.055 Kg
Voltage:
5 to 14 V
Current:
200 mA (Simple Payloads), Up to 650 mA (External)
Power Consumption:
0.015 to 1.4 W
Altitude Stabilization Component:
Magnetometer, Gyroscope, Angular Velocity
Interface:
CAN, SPI, I2C, USB, UART, Ethernet
Space Heritage:
Yes
more info