Satellite On-Board Computers (OBC) - Page 2

56 Satellite On-Board Computers (OBC) from 30 Manufacturers meet your specification.
56 Satellite On-Board Computers (OBC) from 30 Manufacturers
56 Products from 30 Manufacturers
Page 2 of 4
Description:High Performance Fault-Tolerant OBC

Product Specs

Orbit:
LEO
Power Consumption:
3 W
Interface:
UART, RS-485, RS-422, LVDS, Ethernet, CAN, PCle
Space Standard:
ISO-19683
more info
Description:OnBoard Computer for CubeSats and Microsatellites

Product Specs

Satellite Type:
CubeSat, MicroSat
Mass:
0.065 Kg
Voltage:
3.3 to 5 V
Altitude Stabilization Component:
Magnetometer, Accelerometer, Gyroscope, IMU, Sensors
Interface:
CAN, I2C, SPI, UART, RS-422, PCle, RS-485
Space Heritage:
Yes
more info
Description:Reconfigurable Computer for Space Payload Processing

Product Specs

Interface:
PCIe
more info
Description:Single Board Computer for LEO, GEO and Lunar Missions

Product Specs

Orbit:
LEO, MEO, GEO, NEO
Mass:
0.35 Kg
Voltage:
3.3 V
Power Consumption:
12.5 W
Radiation:
100 Krad
Altitude Stabilization Component:
Sensors
Interface:
Ethernet, RS-422, PCle
Space Heritage:
Yes
more info
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Description:LEON-3FT Dual Core to control the satellite flight segment

Product Specs

Power Consumption:
15 to 25 W
Altitude Stabilization Component:
Magnetometer, Gyroscope
Interface:
CAN, SpaceWire
Space Heritage:
Yes
more info
Description:On-Board Computer for Satellites

Product Specs

Satellite Type:
SmallSat, NanoSat, MicroSat
Orbit:
LEO
Voltage:
6 to 14 V
Radiation:
20 Krad
Altitude Stabilization Component:
Sensors
Interface:
CAN, I2C, LVDS, SPI, RS-422, PCle, RS-485, UART, Ethernet, SpaceWire
Space Heritage:
Yes
more info
Description:Space Qualified Processor Unit for Microsatellites

Product Specs

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
Description:Space Qualified Single Board Computer

Product Specs

Voltage:
1.5 to 5 V
Radiation:
100 Krad
Altitude Stabilization Component:
IMU, Sensors, Magnetospheric
Interface:
RS-422, PCle, UART, SPI
Space Heritage:
Yes
Space Standard:
EEE-INST-002
more info
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Description:Satellite On-Board Command & Data Handling Subsystem with Redundancy

Product Specs

Orbit:
LEO
Mass:
4.25 Kg
Voltage:
5 V
Power Consumption:
3 to 5 W
Radiation:
30 Krad
Interface:
CAN, RS-422, RS-485, RS-232, I2C, SPI
more info
Description:On-Board Computer Module for Attitude and Orbit Control

Product Specs

Current:
0.5 to 1.5 A
Interface:
I2C, RS-422, RS-485, SPI, UART, USB, CAN-FD, GigE
more info
Description:Integrated Satellite Avionics Platform

Product Specs

Satellite Type:
CubeSat
Mass:
100 g
Voltage:
5 V, 12 V
Current:
3 A, 3.6 A, 12 A
Power Consumption:
50 to 100 W
Interface:
USB 2.0, I2C
Space Heritage:
Yes
more info
Description:On-Board Computer for CubeSat Missions

Product Specs

Satellite Type:
CubeSat
Interface:
CAN, RS-422, RS-485, UART, USART, I2C, SPI
more info
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Description:Pushing the Boundaries of Fully Radiation Hardened Performance

Product Specs

Voltage:
5 to 18 V
Power Consumption:
0.75 to 100 W
Interface:
UART, CAN, I2C, SPI, RS-422, SpaceWire, LVDS, USB 2.0, Ethernet
more info
Description:OnBoard Computer for Mini and Micro Satellites

Product Specs

Satellite Type:
MicroSat, MiniSat
Mass:
0.150 Kg
Voltage:
8 to 12 V
Current:
50 to 150 mA
Interface:
CAN, RS-422, PCle
more info
Description:Single Board Computer for Image Processing Applications

Product Specs

Satellite Type:
CubeSat
Orbit:
LEO, MEO, GEO
Mass:
0.165 Kg (ProtonX-Box), 0.475 (Proton2X-Box) Kg
Voltage:
28 V
Power Consumption:
8 to 12 W
Radiation:
100 Krad
Interface:
UART, Ethernet, SpaceWire, CAN
Space Heritage:
Yes
more info
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