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Electrical Engineering
Division Code 560 |
Electrical Engineering Division
Code 560, NASA GSFC Greenbelt, Maryland |
Rad-Hard Reconfigurable Field Programmable Gate Array (RHrFPGA),
Code 564
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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