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Electrical Engineering Division
Code 560
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Electrical Engineering Division
Code 560, NASA GSFC Greenbelt, Maryland

Rad-Hard Reconfigurable Field Programmable Gate Array (RHrFPGA), Code 564

Rad-Hard reconfigurable Field Programmable Gate Array (RHrFPGA)

Description

Reconfigurable FPGA’s dramatically decrease development time by reducing the cost of mistakes and by dramatically shortening the update cycle.

Approach

  • RFPHA’s must be SEU hard
    • A single bit flip will change the logic in the part until it is reloaded
    • No good scheme has been discovered to allow use of commercial SEU soft devices in critical space applications, triple voting schemes still require constant verification of internal memory
  • Systems can be reprogrammed after fabrication for a particular application
    • In flight reconfiguration of instruments is possible (desired for NGST camera electronics)
    • Simulation time reduced because parts can be re-used and reload time is minutes not days
  • Designers would always use a re-configurable part instead of a single use part of similar functionality.
    • SWIFT used RFPGA’s for initial rapid prototyping and must redesign for parts which are OK for flight.
  • Properties of the first RHrFPGA part
    • 20,000 gate, RAM based, 100 Mhz, re-configurable FPGA
    • Flight version from Honeywell, commercial equivalent from Atmel
    • Both versions use off-the-shelf Atmel development tools
    • Flight unit is TID, SEU and SEL hard
  • Key enabling technology for Re-configurable Computing (RC) and re-configurable hardware systems
  • Funding profile is limiting development schedule additional partners or funding sources are needed.

Features

  • Integrated X-S transponder: S-band receive at 4 kbps, X-band transmit at 20 Mbps.
  • Integrated PHEMPT power amplifier technology.
  • Compatible with both TDRSS users and direct to Earth users.

Potential Enterprise Benefit

  • Facilitates channelized X-band telemetry downlink with commercial potential
  • Advanced, high efficiency RF amplifier technology reduces power consumption
  • Takes advantage of previous NASA investments (4th generation xpdr, SMEX command receiver) to maximize cost savings

Product

  • Engineering demonstration model - March 2000.
  • Protoflight unit (proposed for NPP bridge mission) available fall 2001
   

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Last Modified: December 5, 2005