Features RS-422 differential Inputs and RS-422 differential Outputs with onboard FPGA logic to interface to the external spacecraft sensors and devices.
Designed for LEO, Mars Terrestrial with an Option for GEO Environments
One (1) IEEE-1394a FireWire OHCI Controller and Three (3) 400Mbps FireWire Ports with Power Management Circuitry
12 RS-422 Input and 12 RS-422 Output Channels can be Configured to NRZ-L, NRZ-M and BiPhase-L Modes
FPGA Control Logic for a Variety of Spacecraft Standard or Custom Data Interfaces
Triple-Voted Algorithm is Provided for Input and Output Data Buffer
Software Configurable Interrupt Capability to Indicate Completion of Pre-defined Tasks
IEEE 1101.2 (Conduction-Cooled) for Both Engineering Unit and Flight Unit
32-bit PCI 2.1 Compliant CompactPCI Interface at 33.333 MHz
Full-Featured 1394 Software Library is Available for VxWorks
S710 Nominal Power Consumption is Less than 3.5 Watts
Level-2 Components per NASA GSFC 311-INST-001A Specification are Available
Features RS-422 differential Inputs and RS-422 differential Outputs with onboard FPGA logic to interface to the external spacecraft sensors and devices.
- Designed for LEO, Mars Terrestrial with an Option for GEO Environments
- One (1) IEEE-1394a FireWire OHCI Controller and Three (3) 400Mbps FireWire Ports with Power Management Circuitry
- 12 RS-422 Input and 12 RS-422 Output Channels can be Configured to NRZ-L, NRZ-M and BiPhase-L Modes
- FPGA Control Logic for a Variety of Spacecraft Standard or Custom Data Interfaces
- Triple-Voted Algorithm is Provided for Input and Output Data Buffer
- Software Configurable Interrupt Capability to Indicate Completion of Pre-defined Tasks
- IEEE 1101.2 (Conduction-Cooled) for Both Engineering Unit and Flight Unit
- 32-bit PCI 2.1 Compliant CompactPCI Interface at 33.333 MHz
- Full-Featured 1394 Software Library is Available for VxWorks
- S710 Nominal Power Consumption is Less than 3.5 Watts
- Level-2 Components per NASA GSFC 311-INST-001A Specification are Available
