Use the following information and links to find quick answers to questions currently facing users of EEE Parts for space missions.

The question of Actel device usage for space missions is a complex question with many variables. What follows below is a brief NEPP recommendation for project usage, for the latest generations of devices.


RTSX-S devices (0.25 um MEC foundry)
These devices have been undergoing investigation for reliability-related issues (NASA/NESC/NEPP/OLD, Aerospace, others). At this time, the critical failure mode is such that device speed is reduced on a single net, from a damaged programmed antifuse. Thus, if you plan on using these devices (as in, already have bought them) , there are several recommendations:

- Utilize most recent programming algorithms for this device, and
- Ensure designs satisfy all specifications (many designs do not).
- Recognize that these devices are extremely ESD sensitive.
- Lot specific DPA for wire bond integrity is recommended.

There are three programming algorithms available: the original programming algorithm, the "new programming algorithm" which addresses one of two classes of antifuse problems found, and the "modified new programming algorithm" which addresses both classes of antifuse problems found.  These improvements appear to mitigate and not eliminate the issue.

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RTSX-SU devices (0.25 um UMC foundry)
These are the "new" RTSX-SU devices for space and have also been undergoing reliability tests (NASA/NESC/NEPP/OLD, Aerospace, others). They, at this point, seem to have improved reliability versus the MEC foundry parts. They are the current "recommended" device for projects that have not yet procured devices. The recommendations are:

- Utilize the most recent programming algorithm available, and
- Ensure designs satisfy all specifications (many designs do not).
- Recognize that these devices are extremely ESD sensitive.
- Lot specific DPA for wire bond integrity is recommended.

There are two programming algorithms.  The first is the original programming algorithm.  The improved programming algorithm is called UMA for "UMC Modified Algorithm."  Also, the routing software is being modified to minimize peak currents through a net using only a "fast connect" called SAL for "S Antifuse Loading."

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RTAX-S devices  (0.15 um UMC foundry)
These are the latest generation space devices from Actel. Reliability testing by Actel has shown promise. However, until independent reliability and radiation tests are performed, we recommend that near-term projects not baseline these devices. This opinion will likely change within 6 months once independent data exists such as that generated for the RTSX family of devices.

All devices:
- More complete single event data is desired on all device types above (high-temp latchup and high-speed single event upset/transient).
- In addition, we recommend lot-specific TID tests be performed. This is standard practice for Actel.
It should also be noted that traditional "good engineering practices" such as clock derating should also be applied.

There is currently debate among the NASA centers on the need for post programming electrical test and post programming burn in.  Proper risk management practices would dictate the need for an independent verification of the programming procedure.  This can only be done via an electrical test on a sophisticated tester with through test vectors.  This needs to be built into planning for cost and schedule well in advance of any testing.  In all cases, particularly if post programming testing and burn in is not conducted, significant operation at use conditions and temperatures for a minimum of 500 hours is recommended.

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