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.

Some SX-S VIH/VIL Data at 125 °C

T25KS001 125C                    
VIL                      
PINNAME 2.3V/
2.3V		 2.5V/
2.5V		 2.7V/
2.7V		 2.3V/
3.0V		 2.5V/
3.3V		 2.7V/
3.6V		 2.3V/
4.5V		 2.3V/
4.75V		 2.5V/
5.0V		 2.7V/
5.25V		 2.7V/
5.50V
FCLKINPUT 1350 1470 1590 1350 1290 1590 1350 1345 1470 1590 1590
FCLKINPUT 1395 1515 1640 1395 1335 1640 1395 1395 1515 1635 1635
FCLKINPUT 1380 1500 1620 1380 1320 1625 1380 1370 1500 1620 1620
FCLKINPUT 1365 1485 1610 1365 1305 1610 1365 1360 1485 1605 1610
FCLKINPUT 1365 1485 1605 1365 1305 1605 1355 1360 1485 1605 1605
                     
Min 1350 1470 1590 1350 1290 1590 1350 1345 1470 1590 1590
Max 1395 1515 1640 1395 1335 1640 1395 1395 1515 1635 1635
                     
                     
VIH                      
PINNAME 2.3V/
2.3V		 2.5V/
2.5V		 2.7V/
2.7V		 2.3V/
3.0V		 2.5V/
3.3V		 2.7V/
3.6V		 2.3V/
4.5V		 2.3V/
4.75V		 2.5V/
5.0V		 2.7V/
5.25V		 2.7V/
5.50V
FCLKINPUT 1265 1370 1480 1240 1165 1450 1225 1225 1340 1445 1430
FCLKINPUT 1305 1415 1525 1275 1210 1495 1265 1265 1380 1480 1475
FCLKINPUT 1295 1400 1510 1265 1195 1480 1255 1260 1370 1475 1460
FCLKINPUT 1275 1385 1495 1245 1185 1475 1245 1245 1355 1460 1450
FCLKINPUT 1275 1385 1490 1245 1180 1465 1240 1245 1355 1455 1445
                     
Min 1265 1370 1480 1240 1165 1450 1225 1225 1340 1445 1430
Max 1305 1415 1525 1275 1210 1495 1265 1265 1380 1480 1475
                     
VIL-VIH 85 100 110 110 125 140 125 120 130 145 160
90 100 115 120 125 145 130 130 135 155 160
85 100 110 115 125 145 125 110 130 145 160
90 100 115 120 120 135 120 115 130 145 160
90 100 115 120 125 140 115 115 130 150 160

 

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Last Revised: February 03, 2010
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