NASA Office of Logic Design

NASA Office of Logic Design

A scientific study of the problems of digital engineering for space flight systems,
with a view to their practical solution.


Independent NASA Test of
Actel SX-A, SX-S, and SX-SU
Field Programmable Gate Arrays (FPGAs)

This page is used for the official dissemination of test status, results, and reports.

Analysis of S/N 50718: Out of family ICCA

Summary:

The mean ICCA for KU1 is 461 µA with a standard deviation of 52 µA.  S/N 50718 read approximately 1.8 mA.  While this value is within the specification value of 25 mA (ICCA + ICCI) the device was removed from the population prior to the beginning of the stress tests.  Preliminary analysis indicates that this is not a programmed antifuse related matter but is an internal short.  ESD is suspected and the failure analysis will be completed.

History

Figure 1. TCK I/O Schematic with FIB pad locations

 

Figure 2, below, shows the following:

Figure 2. ESD Damage at Primary site

Figure 3A, below, shows the following:

Figure 3A. ESD Damage at secondary site (1 of 2)

Figure 3B, below, shows the following:

Figure 3B. ESD Damage at secondary site (2 of 2)

 

NASA Test Home Page


Home - NASA Office of Logic Design
Last Revised: February 28, 2005
Digital Engineering Institute
Web Grunt: Richard Katz
NACA Seal