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.


CX2041 SEE Data (5V) @ BNL Sep., 1997

 

CX2041 Test Data Table

Run # Run ID Bias Voltage Effective LET (MeV-cm2/mg) Fluence (ions/cm2) Latch Comments
R35 CX1T1 5.5 18.8 107 No 7 Upsets
R38 CX2T1 5.5 18.8 107 No 2 Upsets
R37 CX1T3 5.5 22.0 Yes Moderate Quick Latch
R40 CX2T3 5.5 22.0 Yes Immediate Latch
R36 CX1T2 5.5 26.5 Yes Quick Latch
R39 CX2T2 5.5 26.5 Yes Immediate Latch
R10 CX1B1 4.5 37.1 Yes
R11 CX1B2 4.5 37.1 Yes Immediate Latch
R12 CX2B1 4.5 37.1 Yes Immediate Latch

 

The SEL threshold for this lot of parts is approximately 20 MeV-cm2/mg.   Latch currents ranged from ~ 150 mA to > 800 mA.

The SEU threshold was not found for this lot but a small cross-section was measured at an LET of 18 MeV-cm2/mg.  This DUT pattern utilized 1,200 flip-flops so a single cross-section measurement, at an LET of 18 MeV-cm2/mg, is: 0.4 x 10-9 cm2/flip-flop.


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