A scientific study of the problems of
digital engineering for space flight systems,
with a view to their practical solution.
This is a test of the A54SX16A, 0.22 µm, UMC die. This test was run with minimal supply voltages, 3.0/2.25 for all runs. All runs resulted in what appeared to be single event latchup (SEL). An LET of 15 MeV-cm2/mg (Chlorine) was the minimum LET used in this test set.
Package: PQ208
Serial Nos. LAN6101, LAN6102
L/C: DPF491
Test frequency: 1 MHz.
DUT schematics: MKJ911
Total Number of Flip-flops: N/A, SEL, antifuse test.
Clock Configuration: N/A
Antifuse rupture: N/A, all runs resulted in SEL.
SEL: Detected.
Loss of control, i.e., JTAG upset: N/A, all runs resulted in SEL.
All runs resulted in latchup with a bias of 3.0/2.25 volts.
Run # DeviceID Ion Energy
(MeV)Range
(µm)LET(Si)
MeV-cm2/mgTilt
(deg)Strip Chart 377 6102 Cl-35 95 25.96 15.47 0 374 6102 Cl-35 95 22.49 17.86 30 6102c2.pdf 375 6102 Cl-35 95 22.49 17.86 30 6102c3.pdf 373 6102 Cl-35 95 18.36 21.88 45 6102c1.pdf 369 6101 Br-81 278.5 36.03 37.46 0 6101b1.pdf 370 6101 Br-81 278.5 36.03 37.46 0 6101b2.pdf 371 6101 Br-81 278.5 36.03 37.46 0 6101b3.pdf 372 6102 Br-81 278.5 36.03 37.46 0 6102b1.pdf
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Last Revised January 09, 2002
Digital Engineering Institute
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