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AM26LS31MW/883 Datenblatt(PDF) 3 Page - Texas Instruments |
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AM26LS31MW/883 Datenblatt(HTML) 3 Page - Texas Instruments |
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3 / 14 page ![]() DS26LS31MQML www.ti.com SNOSAM5B – AUGUST 2005 – REVISED APRIL 2013 Radiation Features DS26LS31MEFQML 300 Krads (Si) DS26LS31MJFQML 300 Krads (Si) DS26LS31MJFQMLV 300 Krads (Si) DS26LS31MWFQML 300 Krads (Si) DS26LS31MWFQMLV 300 Krads (Si) Quality Conformance Inspection MIL-STD-883, Method 5005 - Group A Subgroup Description Temp (°C) 1 Static tests at +25 2 Static tests at +125 3 Static tests at -55 4 Dynamic tests at +25 5 Dynamic tests at +125 6 Dynamic tests at -55 7 Functional tests at +25 8A Functional tests at +125 8B Functional tests at -55 9 Switching tests at +25 10 Switching tests at +125 11 Switching tests at -55 DS26LS31M - SMD, QMLV & RH Electrical Characteristics DC Parameters The following conditions apply, unless otherwise specified. +V = 5V, VCM = 0V. (1) Sub- Parameter Test Conditions Notes Min Max Unit groups See and(2) VIH Logical "1" Input Voltage VCC = 4.5V 2 V 1, 2, 3 (3) See(2) and VIL Logical "0" Input Voltage VCC = 5.5V .8 V 1, 2, 3 (3) VOH Logical "1" Output Voltage VCC = 4.5V, IOH = -20mA See(3) 2.5 V 1, 2, 3 VOL Logical "0" Output Voltage VCC = 4.5V, IOL = 20mA See(3) .5 V 1, 2, 3 IIH Logical "1" Input Current VCC = 5.5V, VIN= 2.7V See(3) -2.0 20 uA 1, 2, 3 IIL Logical "0" Input Current VCC = 5.5V, VIN = .4V See(3) 100 -360 uA 1, 2, 3 II Input Reverse Current VCC = 5.5V, VIN = 7V See(3) -.01 .1 mA 1, 2, 3 VCC = 5.5V, VO = .5V See(3) -20 uA 1, 2, 3 IO TRI-STATE Output Current VCC = 5.5V, VO = 2.5V See(3) 20 uA 1, 2, 3 VIC Input Clamp Voltage VCC = 4.5V, IIN = -18mA See(3) -1.5 V 1, 2, 3 IOS Output Short Circuit Current VCC = 5.5V See(3) -30 -150 mA 1, 2, 3 VCC = 5.5V, All Outputs Disabled or ICC Power Supply Current See(3) 80 mA 1, 2, 3 Active (1) Pre and post irradiation limits are identical to those listed under AC and DC electrical characteristics. These parts may be dose rate sensitive in a space environment and demonstrate enhanced low dose rate effect. Radiation end point limits for the noted parameters are ensured only for the conditions as specified in MIL-STD 883, Method 1019, Condition A. (2) Parameter tested go-no-go only. (3) Subgroups 1, 2 and 9, 10: Power dissipation must be externally controlled at elevated temperatures. Copyright © 2005–2013, Texas Instruments Incorporated Submit Documentation Feedback 3 Product Folder Links: DS26LS31MQML |
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