OBC-1 - CAVU Aerospace UK - Smallsat Catalog - Orbital Transports

OBC-1

The CAVU OBC-1 is a highly reliable and efficient FPGA-based satellite computing system that is state-of-the-art. It is designed to ensure smooth and uninterrupted operation during critical space missions. The system has flexible architecture that allows it to be easily scaled up with the same module to make a redundant satellite computer.

This powerful computer system offers a host of features and benefits that make it an ideal choice for space operations. It is designed to withstand a wide range of space environments and ensures that your satellite payload runs smoothly with precise timing, high throughput, and low power consumption.

Specifications
Dimensions:
160x100 mm
Mass:
75 g
Power Supply:
5V +/- 5%
Power Consumption:
1W ~ 2W
Processor:
ARM Cortex-M3 on FPGA
FPGA:
Microchip/Microsemi SmartFuion2 Flash Based FPGA
Processor Performance:
150 DMIPS @ 128MHz
Programming and Debug:
SoftConsole or Keil via JTAG
RAM:
80Mbits MRAM 40 bits width (64Mbits+16Mbits ECC)
ROM:
48Mbits MRAM (Configurable as Triple 16Mbits)
Nonvolatile Flash Memory:
Total 96Gbit SLC NAND Flash (Triple 32G)
Serial FRAM:
256 Kbit
Serial NOR:
256Mbit
Interface:
Digital Outputs (5V/3.3V): 70x
Interface:
Digital Inputs (5V/3.3V): 30x
Interface:
16bits Analog to Digital Converter (-10V ~ +10V) : 32
Interface:
12bits Digital to Analog Converter (0V~5V) : 2
Serial Interface:
CAN2.0 Up to 1Mbps : 4x
Serial Interface:
Full-Duplex RS422 : 1x
Serial Interface:
Half-Duplex RS485 : 2x
Serial Interface:
RS232 : 1x
Serial Interface:
I2C : 1x
Serial Interface:
SPI : 1x
Radiation Hardness:
Total Ionizing Dose: 30Krad (Si)/yr
Latchup:
SEE @ 60MeV
Operating Temperature Range:
-40C to 85˚C @10^-8 torr
Shock:
2000g, 2000-10000Hz
Random Vibrations:
14g(RMS) 3-Axis , 20~2000Hz
Expected Life-time:
3-5 years in LEO
Feature:
On-Board Current & Temperature Monitoring
Feature:
On-Board Watchdog
Feature:
Triple Real Time Clock
Feature:
Hot Redundant On-Board Voltage Converters
Documents